2024-03-28T16:13:36Z
https://zenodo.org/oai2d
oai:zenodo.org:546709
2020-01-20T17:19:45Z
user-ewade
Ciampa, Pier Davide
Nagel, Björn
Rajpal, Darwin
La Rocca, Gianfranco
2013-09-18
<p>The work presents a collaborative design approach, developed to account for the structure flexibility effects in the pre-design stages of generic aircraft configurations. A streamlined design process is developed between DLR and TU Delft, to support the transition from an initial aircraft conceptual solution, to physics based simulations. The TU Delft DEE initiator is the conceptual tool providing the initial design, which is used to instantiate further analysis tool. An Aeroelastic Engine module is responsible for the abstraction of the aircraft structural properties, and the generation of the fluid-structure disciplinary couplings, necessary to account for the flexibility effects. Multiple distributed disciplinary solvers are available, and accessible via a decentralized architecture. All the analysis modules are integrated in the design workflow by means of the open source distributed framework RCE, and the DLR’s central data model CPACS. The approach is tested for the pre-design of a conventional aircraft and a box-wing configuration, designed for a set of top level aircraft requirements. Hence, the flexibility effects for both cases are presented. The results demonstrate the importance of accounting for the flexibility effects already in the pre-design phase, especially in case of box-wing configurations, where difference in design performance can occur when ignoring such effects.</p>
http://EWADE.AircraftDesign.org --- http://ProceedingsEWADE2013.AircraftDesign.org
https://doi.org/10.5281/zenodo.546709
oai:zenodo.org:546709
Zenodo
https://zenodo.org/communities/ewade
https://doi.org/
info:eu-repo/semantics/openAccess
Creative Commons Attribution 4.0 International
https://creativecommons.org/licenses/by/4.0/legalcode
EWADE 2013, CEAS 2013, 11th European Workshop on Aircraft Design Education --- 4th CEAS Air & Space Conference, Linköping, Sweden, 17.-19.09.2013
CPACS
collaborative design
DEE Initiator
aeroelastic engine
OAD
aircraft
design
Europe
workshop
EWADE2013
CEAS2013
Preliminary Design for Flexible Aircraft in a Collaborative Environment
info:eu-repo/semantics/conferencePaper
oai:zenodo.org:546634
2020-01-20T17:03:20Z
user-ewade
Jouannet, C
Berry, P
Melin, D
Lundström, D.
2013-09-18
<p>The presented work considers designing, building and flight test of a demonstrator of a personal jet aircraft realized as a student project. The goal is to allow student to participate in an aircraft project from design to flight test in order to acquire aircraft design knowledge from theoretical and practical means. A first theoretical part consists of creating a sizing program for studying different concepts. Then the gathered knowledge will result in the realization of a flying demonstrator. This was realized during a student project over a 5 month period.</p>
http://EWADE.AircraftDesign.org --- http://ProceedingsEWADE2013.AircraftDesign.org
https://doi.org/10.5281/zenodo.546634
oai:zenodo.org:546634
Zenodo
https://zenodo.org/communities/ewade
https://doi.org/
info:eu-repo/semantics/openAccess
Creative Commons Attribution 4.0 International
https://creativecommons.org/licenses/by/4.0/legalcode
EWADE 2013, CEAS 2013, 11th European Workshop on Aircraft Design Education --- 4th CEAS Air & Space Conference, Linköping, Sweden, 17.-19.09.2013
EWADE2013
CEAS2013
student
project
demonstrator
aircraft
design
teaching
education
university
Europe
workshop
Personal Jet - A Student Project
info:eu-repo/semantics/conferencePaper
oai:zenodo.org:546616
2020-01-20T17:40:09Z
openaire
user-ewade
La Rocca, G.
2013-09-18
<p>TU Delft Faculty of Aerospace Engineering: The <strong>Faculty of Aerospace Engineering</strong> at the Delft University of Technologyin the Netherlands is the merger of two interrelated disciplines, aeronauticalengineering and astronautical engineering. The Faculty is one of the largest of the eight faculties at TU Delft and one of the largest faculties devoted entirely to aerospace engineering in northern Europe. It is the only institute carrying out research and education directly related to aerospace engineering in the Netherlands. Through the years, the Faculty has responded to the increasing demands of the aerospace industry by further expanding its facilities and laboratories. Today the Faculty has a student body of approximately 2300 undergraduates and graduates, 237 members of academic staff and 181 PhD students.<span> </span>Around 34% of the student population is from outside the Netherlands. Extensive laboratory and testing facilities are used in research and teaching. The facilities include supersonic, hypersonicand subsonic wind-tunnels, a high-sensitivity navigation simulator, and a materials testing laboratory. These facilities make it possible to conduct experiments in man-machine factors, flight control, structures and materials, aerodynamics, simulation, motion and navigation. The faculty owns and makes use of a Cessna Citation jet aeroplane which is a unique flying laboratory.</p>
http://EWADE.AircraftDesign.org --- http://ProceedingsEWADE2013.AircraftDesign.org
https://doi.org/10.5281/zenodo.546616
oai:zenodo.org:546616
Zenodo
https://zenodo.org/communities/ewade
https://doi.org/
info:eu-repo/semantics/openAccess
Creative Commons Attribution 4.0 International
https://creativecommons.org/licenses/by/4.0/legalcode
EWADE 2013, 11th European Workshop on Aircraft Design Education, Linköping, Sweden, 17.-19.09.2013
EWADE2013
aircraft
design
teaching
education
research
university
Europe
workshop
Aerospace Engineering at TU Delft
info:eu-repo/semantics/lecture
oai:zenodo.org:6038482
2022-02-11T01:49:32Z
openaire
user-ewade
Kretov, Anatolii
2020-10-21
<p><strong>Purpose</strong> – The purpose of this work is to further develop the methodology for calculating the aircraft take-off-mass and its main functional components for the conceptual analysis and synthesis of new projects.</p>
<p><strong>Design/methodology/approach</strong> – The method is based on the assessment of changes in the take-off gross mass (TOGM) of the already developed project or already existing a basic version of the aircraft when making local mass changes for its modification or for the numerical researches to create a more advanced project. The method is based on the "Sensitivity factors of mass" (SFM) of aircraft, which represents the ratio of TOGM to initial (local) mass changes of its main functional components. The method of analytical refined calculation of SFM for the initial mass change and the main aerodynamic characteristics is given.</p>
<p><strong>Findings</strong> – In comparison with the long-known method based on weight (mass) growth factors, which were considered constant, this method takes into account the dependence from the value of the initial local mass change and its functional purpose.</p>
<p><strong>Practical implications</strong> – This method allows the designer to calculate more strictly the final changes in the TOGM on the initial stages of conceptual design when finding new project solutions. Numerical calculations are given on the example of passenger aircraft. The dependence of SFM, and TOGM and its functional masses on the value of the initial change of the structure mass is shown.</p>
<p><strong>Originality/value</strong> – The considered method based on SFM is simple and convenient, and more accurate for conducting project research on many project parameters when analyzing and synthesizing a new project.</p>
http://EWADE.AircraftDesign.org --- http://Presentations2020.AircraftDesign.org
https://doi.org/10.5281/zenodo.6038482
oai:zenodo.org:6038482
eng
Zenodo
https://zenodo.org/communities/ewade
https://doi.org/10.5281/zenodo.6038481
info:eu-repo/semantics/openAccess
Creative Commons Attribution 4.0 International
https://creativecommons.org/licenses/by/4.0/legalcode
EWADE/READ 2020, 15th European Workshop on Aircraft Design Education, Rzeszów, Poland / Online, 21.-22.10.2020
EWADE2020
Conceptual Design
Sensitivity Factors
Aircraft
Take-Off Mass
Sensitivity Factors of Aircraft Mass for the Conceptual Design
info:eu-repo/semantics/lecture
oai:zenodo.org:4159133
2023-11-24T21:16:37Z
openaire
user-ewade
user-profscholz
Scholz, Dieter
2020-10-21
<p>Purpose – Establish a "journal" for the aircraft design community. --- Approach – Aircraft design is too small as a topic for a journal. Use a continuous Special Issue i.e. only a subset of a journal. Follow the Open Access publishing model that can life already on a low number of papers annually. --- Findings – The well established publisher MDPI published already one Special Issue "Aircraft Design" in "Aerospcae" (ISSN 2226-4310) and was willing to follow the approach. The journal has a CiteScore (2019) of 2.6 from Scopus and is part of the Emerging Sources Citation Index - Web of Science (Clarivate Analytics). --- Tradition – The tradition of the journal Aircraft Design at Elsevier (ISSN: 1369-8869) which was published from 1998 to 2001 with Prof. Egbert Torenbeek and Prof. Dr. Jan Roskam as Editors is continued. --- Limitations – Article Processing Charges (APC) have to be paid. A large discount is available for authors from EWADE/SCAD and READ. Further discounts are granted based on reviews. --- Originality and Value – This is the only "journal" fully dedicated to aircraft design.</p>
http://EWADE.AircraftDesign.org --- http://Presentations2020.AircraftDesign.org
https://doi.org/10.5281/zenodo.4159133
oai:zenodo.org:4159133
eng
Zenodo
https://zenodo.org/communities/profscholz
https://zenodo.org/communities/ewade
https://doi.org/10.5281/zenodo.4159132
info:eu-repo/semantics/openAccess
Creative Commons Attribution Non Commercial Share Alike 4.0 International
https://creativecommons.org/licenses/by-nc-sa/4.0/legalcode
EWADE/READ 2020, 15th European Workshop on Aircraft Design Education, Rzeszów, Poland / Online, 21.-22.10.2020
EWADE2020
aerospace
aviation
aircraft
design
publishing
journal
Open Access
Prof. Scholz @ Zenodo
The Continuous Special Issue "Aircraft Design" of the Open Access Journal "Aerospace" at MDPI
info:eu-repo/semantics/lecture
oai:zenodo.org:21443
2020-01-20T14:54:03Z
openaire
user-ewade
Obert, Ed
2013-09-18
<p>An analysis is described of side-force and yawing-moment-in-sideslip of conventional transport aircraft based on available wind tunnel and full-size aircraft data. After a chapter on general design requirements the analysis is divided in a part which describes the tail-off characteristics and a part which describes the contribution of the tail surfaces to side-force and yawing-moment-due-to-sideslip. Particular attention is paid to the drfferent contributions to the sidewash as expenenced by the tail surfaces. Also rudder characteristics are discussed.</p>
http://EWADE.AircraftDesign.org --- http://ProceedingsEWADE2013.AircraftDesign.org
https://doi.org/10.5281/zenodo.21443
oai:zenodo.org:21443
Zenodo
https://zenodo.org/communities/ewade
https://doi.org/
info:eu-repo/semantics/openAccess
Creative Commons Attribution 4.0 International
https://creativecommons.org/licenses/by/4.0/legalcode
EWADE 2013, 11th European Workshop on Aircraft Design Education, Linköping, Sweden, 17.-19.09.2013
stability
static directional stability
control
transport
aircraft
side force
yaw
sideslip
wind tunnel
tail
wing
sidewash
rudder
EWADE2013
Static Directional Stability and Control of Transport Aircraft
info:eu-repo/semantics/lecture
oai:zenodo.org:18916
2020-01-20T15:06:35Z
openaire
user-ewade
Torenbeek, Egbert
2013-09-18
<p>Presentation on the occasion of the new book:</p>
<p>"Advanced Aircraft Design: Conceptual Design, Analysis and Optimization of Subsonic Civil Airplanes".</p>
<p>Author: Egbert Torenbeek</p>
<p>Published Online: 27 MAY 2013</p>
<p>Print ISBN: 9781118568118</p>
<p>Online ISBN: 9781118568101</p>
<p>DOI: 10.1002/9781118568101</p>
http://EWADE.AircraftDesign.org --- http://ProceedingsEWADE2013.AircraftDesign.org
https://doi.org/10.5281/zenodo.18916
oai:zenodo.org:18916
Zenodo
https://zenodo.org/communities/ewade
https://doi.org/
info:eu-repo/semantics/openAccess
Creative Commons Attribution 4.0 International
https://creativecommons.org/licenses/by/4.0/legalcode
EWADE 2013, 11th European Workshop on Aircraft Design Education, Linköping, Sweden, 17.-19.09.2013
aircraft
design
optimization
subsonic
civil
airplane
aeroplane
EWADE2013
The New Textbook ”Advanced Aircraft Design – Conceptual Design, Technology and Optimization of Subsonic Civil Airplanes“
info:eu-repo/semantics/lecture
oai:zenodo.org:546412
2020-01-20T13:02:53Z
openaire
user-ewade
Jouannet, Christopher
2013-09-18
<p>Challenges within Aircraft design. Student's project, why? Project requirements. Concepts. Design. Manufacturing. First flight.</p>
http://EWADE.AircraftDesign.org --- http://ProceedingsEWADE2013.AircraftDesign.org
https://doi.org/10.5281/zenodo.546412
oai:zenodo.org:546412
Zenodo
https://zenodo.org/communities/ewade
https://doi.org/
info:eu-repo/semantics/openAccess
Creative Commons Attribution 4.0 International
https://creativecommons.org/licenses/by/4.0/legalcode
EWADE 2013, 11th European Workshop on Aircraft Design Education, Linköping, Sweden, 17.-19.09.2013
EWADE2013
aircraft
design
teaching
education
research
university
Europe
workshop
MidJet a Personal Jet - A Student Project
info:eu-repo/semantics/lecture
oai:zenodo.org:6037723
2022-02-12T18:38:05Z
openaire
user-ewade
SAE Aero Design Team
Muchla, Grzegorz
2020-10-21
<p>The SAE Aero Design competition is a real-world design challenge designed to compress a typical aircraft development program into one calendar year, taking participants through the system engineering process of breaking down requirements. It exposes participants to the nuances of conceptual design, manufacturing, system integration/test, and sell-off through demonstration. Warsaw University of Technology participated in the SAE Aero Design competition (West) in 2020. Here are a few impressions.</p>
http://EWADE.AircraftDesign.org --- http://Presentations2020.AircraftDesign.org
https://doi.org/10.5281/zenodo.6037723
oai:zenodo.org:6037723
eng
Zenodo
https://zenodo.org/communities/ewade
https://doi.org/10.5281/zenodo.6037722
info:eu-repo/semantics/openAccess
Creative Commons Attribution 4.0 International
https://creativecommons.org/licenses/by/4.0/legalcode
EWADE/READ 2020, 15th European Workshop on Aircraft Design Education, Rzeszów, Poland / Online, 21.-22.10.2020
EWADE2020
SAE Aero Design Competition
info:eu-repo/semantics/lecture
oai:zenodo.org:546442
2020-01-20T13:35:59Z
openaire
user-ewade
La Rocca, G.
van der Linden, P.
Li, M.
2013-09-18
<p>In the RECREATE (REsearch on a CRuiser Enabled Air Transport Environment) project, European research institutes, universities and small businesses work together to investigate a future air transportation system based on the concept. In Flight Refueling (IFR) operations for passenger aircraft is actually one of the two main concepts addressed by RECREATE.</p>
http://EWADE.AircraftDesign.org --- http://ProceedingsEWADE2013.AircraftDesign.org
https://doi.org/10.5281/zenodo.546442
oai:zenodo.org:546442
Zenodo
https://zenodo.org/communities/ewade
https://doi.org/
info:eu-repo/semantics/openAccess
Creative Commons Attribution 4.0 International
https://creativecommons.org/licenses/by/4.0/legalcode
EWADE 2013, 11th European Workshop on Aircraft Design Education, Linköping, Sweden, 17.-19.09.2013
EWADE2013
aircraft
design
teaching
education
research
university
Europe
workshop
Conceptual Design of Passenger Aircraft for In-Flight Refueling Operations
info:eu-repo/semantics/lecture
oai:zenodo.org:546612
2020-01-20T14:58:39Z
openaire
user-ewade
Chaitanya.M.V, Raghu
Staack, Ingo
Krus, Petter
2013-09-18
<p>Aim: XML based multidisciplinary tool integration in a conceptual aircraft design framework. Instead of a "One-tool” a "One-database” approach. Design Automation for fast realization of the concept. To support Conceptual to Preliminary Aircraft design. Conclusions: Multidisciplinary conceptual aircraft design analysis based on a central parametric XML database database. This database -containing all project related data- is intended to grow simultaneously with the refined specification of the airplane. The unified geometry makes meshing easier and serves for no aperture for high fidelity CFD.</p>
http://EWADE.AircraftDesign.org --- http://ProceedingsEWADE2013.AircraftDesign.org
https://doi.org/10.5281/zenodo.546612
oai:zenodo.org:546612
Zenodo
https://zenodo.org/communities/ewade
https://doi.org/
info:eu-repo/semantics/openAccess
Creative Commons Attribution 4.0 International
https://creativecommons.org/licenses/by/4.0/legalcode
EWADE 2013, 11th European Workshop on Aircraft Design Education, Linköping, Sweden, 17.-19.09.2013
EWADE2013
aircraft
design
teaching
education
research
university
Europe
workshop
Integrated Aircraft Design Network
info:eu-repo/semantics/lecture
oai:zenodo.org:546610
2020-01-20T17:09:15Z
openaire
user-ewade
Moerland, Erwin
Becker, Richard-Gregor
Nagel, Björn
2013-09-18
<p>Conclusion: Build up of low-level toolkit. Initial application: combining a/c and engine predesign. Modularly applicable components & attitude change. Translate knowledge between team members having various backgrounds. Clear and streamlined communication, combined implicit and explicit knowledge.</p>
http://EWADE.AircraftDesign.org --- http://ProceedingsEWADE2013.AircraftDesign.org
https://doi.org/10.5281/zenodo.546610
oai:zenodo.org:546610
Zenodo
https://zenodo.org/communities/ewade
https://doi.org/
info:eu-repo/semantics/openAccess
Creative Commons Attribution 4.0 International
https://creativecommons.org/licenses/by/4.0/legalcode
EWADE 2013, 11th European Workshop on Aircraft Design Education, Linköping, Sweden, 17.-19.09.2013
EWADE2013
aircraft
design
teaching
education
research
university
Europe
workshop
Collaborative understanding of disciplinary correlations using a low-fidelity physics based aerospace toolkit
info:eu-repo/semantics/lecture
oai:zenodo.org:546423
2020-01-20T16:19:27Z
openaire
user-ewade
Stumpf, Eike
2013-09-18
<p>Aircraft design /technology integration and assessment represents main research field at ILR. In ILR lecture Fixed Wing Aircraft I: students will work on old aircraft concepts to build up „system thinking“. In ILR lecture Fixed Wing Aircraft II: students will execute a full design cycle to build up „system knowledge“. In ILR lecture Computer‐Aided Aircraft Design: students get familiarized with current conceptual aircraft design tool. C++ tool templates enable to motivate students to do tool development (which otherwise would refuse).</p>
http://EWADE.AircraftDesign.org --- http://ProceedingsEWADE2013.AircraftDesign.org
https://doi.org/10.5281/zenodo.546423
oai:zenodo.org:546423
Zenodo
https://zenodo.org/communities/ewade
https://doi.org/
info:eu-repo/semantics/openAccess
Creative Commons Attribution 4.0 International
https://creativecommons.org/licenses/by/4.0/legalcode
EWADE 2013, 11th European Workshop on Aircraft Design Education, Linköping, Sweden, 17.-19.09.2013
EWADE2013
aircraft
design
teaching
eduction
research
university
Europe
workshop
Aircraft Design Lectures at RWTH Aachen University, Germany
info:eu-repo/semantics/lecture
oai:zenodo.org:546615
2020-01-20T14:38:31Z
openaire
user-ewade
Ciampa, Pier Davide
Nagel, Björn
Rajpal, Darwin
La Rocca, Gianfranco
2013-09-18
<p>Conclusions: - Collaborative design approach for aircraft in pre-design: Enabling physics based analysis. Focus on flexibility effects.<br>
- Integration of distributed physics based modules: Analysis starting from an initial OAD synthesis model. Disciplinary modules for aero-structural design and new synthesis. Flexibility loop influence. - Design cases: Conventional aircraft behaves as expected. Care has to be considered with the unconventional aircraft case. - Outlook: Adopt the approach for design and optimization applications.</p>
http://EWADE.AircraftDesign.org --- http://ProceedingsEWADE2013.AircraftDesign.org
https://doi.org/10.5281/zenodo.546615
oai:zenodo.org:546615
Zenodo
https://zenodo.org/communities/ewade
https://doi.org/
info:eu-repo/semantics/openAccess
Creative Commons Attribution 4.0 International
https://creativecommons.org/licenses/by/4.0/legalcode
EWADE 2013, 11th European Workshop on Aircraft Design Education, Linköping, Sweden, 17.-19.09.2013
EWADE2013
aircraft
design
teaching
education
research
university
Europe
workshop
Preliminary Design for Flexible Aircraft in a Collaborative Environment
info:eu-repo/semantics/lecture
oai:zenodo.org:3752258
2023-11-24T21:29:41Z
openaire
user-ewade
user-profscholz
Scholz, Dieter
Sousa, Tahir
2013-09-19
<p>A 3D visualization is missing for many aircraft preliminary sizing tools. NASA’s Open Vehicle Sketch Pad (OpenVSP) is easy to use, but lacks an interface to input consistent aircraft data. Such an interface has been programmed and is called OpenVSP-Connect. Aircraft are sketched from about 50 parameters. If these are not known to the user, the interface calculates them as good as possible based on simple equations from aircraft design or statistics. Taken this to the extreme, a decent looking aircraft is drawn from as few as two or three input parameters.</p>
http://EWADE.AircraftDesign.org --- http://ProceedingsEWADE2013.AircraftDesign.org
https://doi.org/10.5281/zenodo.3752258
oai:zenodo.org:3752258
Zenodo
https://zenodo.org/communities/profscholz
https://zenodo.org/communities/ewade
https://doi.org/10.5281/zenodo.796593
info:eu-repo/semantics/openAccess
Creative Commons Attribution 4.0 International
https://creativecommons.org/licenses/by/4.0/legalcode
EWADE 2013, 11th European Workshop on Aircraft Design Education, Linköping, Sweden, 17.-19.09.2013
EWADE2013
aircraft
design
sizing
conceptual
open
sketch
interface
Excel
NASA
teaching
education
research
Europe
workshop
2013
Prof. Scholz @ Zenodo
OpenVSP-Connect - Visualize Your Aircraft Sizing Results with NASA's Vehicle Sketch Pad
info:eu-repo/semantics/lecture
oai:zenodo.org:546649
2024-02-29T10:38:10Z
user-ewade
user-profscholz
Scholz, Dieter
2013-09-18
<p>The first Open Access (OA) peer reviewed online journals in aerospace were all established after 2007. Still today more and more OA aerospace journals get started. Many publishers are located in less developed countries. The benefits of OA publishing are undisputed in the academic community, but there is disagreement if the new publishers can work to required standards. The current situation is evaluated based on an Internet review. OA journals in aerospace are listed with their major characteristics. Well known OA publishers charge high publication fees, whereas less known OA publishers tend to charge relatively low fees. All publishers need to be carefully checked for their level of rigor in peer review and their offered service in the scholarly publication process. Authors should evaluate OA journals and publishers against provided lists of criteria before submitting their work.</p>
http://EWADE.AircraftDesign.org --- http://ProceedingsEWADE2013.AircraftDesign.org
https://doi.org/10.5281/zenodo.546649
oai:zenodo.org:546649
Zenodo
https://zenodo.org/communities/profscholz
https://zenodo.org/communities/ewade
https://doi.org/
info:eu-repo/semantics/openAccess
Creative Commons Attribution 4.0 International
https://creativecommons.org/licenses/by/4.0/legalcode
EWADE 2013, CEAS 2013, 11th European Workshop on Aircraft Design Education --- 4th CEAS Air & Space Conference, Linköping, Sweden, 17.-19.09.2013
aerospace
paper
journal
publisher
open access
aircraft
research
university
Europe
EWADE2013
CEAS2013
2013
Prof. Scholz @ Zenodo
Open Access Publishing in Aerospace – Opportunities and Pitfalls
info:eu-repo/semantics/conferencePaper
oai:zenodo.org:546443
2020-01-20T17:14:03Z
openaire
user-ewade
di Meo, Giovanni Antonio
Scholz, Dieter
Fioriti, Marco
Furlan, Andrea
Chiesa, Sergio
2013-09-18
<p>1 - Introduction to MARGARET</p>
<p>2 - MARGARET Aircraft Technologies</p>
<p>3- MARGARET Consortium: Collaboration among Universities and Educational Initiatives</p>
<p>4 - Future of MARGARET</p>
<p> </p>
http://EWADE.AircraftDesign.org --- http://ProceedingsEWADE2013.AircraftDesign.org
https://doi.org/10.5281/zenodo.546443
oai:zenodo.org:546443
Zenodo
https://zenodo.org/communities/ewade
https://doi.org/
info:eu-repo/semantics/openAccess
Creative Commons Attribution 4.0 International
https://creativecommons.org/licenses/by/4.0/legalcode
EWADE 2013, 11th European Workshop on Aircraft Design Education, Linköping, Sweden, 17.-19.09.2013
EWADE2013
aircraft
design
teaching
education
research
university
Europe
workshop
MARGARET: A Personal Transportation Aircraft of Tomorrow Used Today for Collaboration among Universities
info:eu-repo/semantics/lecture
oai:zenodo.org:546697
2020-01-20T14:22:06Z
user-ewade
Chaitanya. M. V, Raghu
Staack, Ingo
Krus, Petter
2013-09-18
<p>This paper describes the XML based multidisciplinary tool integration in a conceptual aircraft design framework, developed by the Division of Fluid and Mechatronic Systems (FluMeS), Linköping University. Based on a parametric data definition in XML, this approach allows for a full 3D CAD integration. The one-database approach, also conducted by many research organizations, enables the flexible and efficient integration of the different multidisciplinary processes during the whole conceptual design phase. This central database approach with a detailed explanation of the developed geometry description and the data processing, focusing on the CAD integration is presented. Application examples of the framework are presented showing the data build up and data handling.</p>
http://EWADE.AircraftDesign.org --- http://ProceedingsEWADE2013.AircraftDesign.org
https://doi.org/10.5281/zenodo.546697
oai:zenodo.org:546697
Zenodo
https://zenodo.org/communities/ewade
https://doi.org/
info:eu-repo/semantics/openAccess
Creative Commons Attribution 4.0 International
https://creativecommons.org/licenses/by/4.0/legalcode
EWADE 2013, CEAS 2013, 11th European Workshop on Aircraft Design Education --- 4th CEAS Air & Space Conference, Linköping, Sweden, 17.-19.09.2013
aircraft conceptual design
parametric modeling
knowledge based
sizing
XML
database
aircraft
design
Europe
workshop
EWADE2013
CEAS2013
Integrated Aircraft Design Network
info:eu-repo/semantics/conferencePaper
oai:zenodo.org:4159259
2023-11-24T21:15:35Z
openaire
user-ewade
user-profscholz
Cheema, John Singh
Scholz, Dieter
2020-10-21
<p><strong>Purpose</strong> – This project work shows a literature survey, clearly defines the mass growth factor, shows a mass growth iteration, and derives an equation for a direct calculation of the factor (without iteration). Definite values of the factor seem to be missing in literature. To change this, mass growth factors are being calculated for as many of the prominent passenger aircraft as to cover 90% of the passenger aircraft flying today. The dependence of the mass growth factor on requirements and technology is examined and the relation to Direct Operating Costs (DOC) is pointed out. >>></p>
<p><strong>Methodology</strong> – Calculations start from first principles. Publically available data is used to calculate a list of mass growth factors for many passenger aircraft. Using equations and the resulting relationships, new knowledge and dependencies are gained. >>></p>
<p><strong>Findings</strong> – The mass growth factor is larger for aircraft with larger operating empty mass ratio, smaller payload ratio, larger specific fuel consumption (SFC), and smaller glide ratio. The mass growth factor increases much with increasing range. The factor depends on an increase in the fixed mass, so this is the same for the payload and empty mass. The mass growth factor for subsonic passenger aircraft is on average 4.2, for narrow body aircraft 3.9 and for wide body aircraft (that tend to fly longer distance) 4.9. In contrast supersonic passenger aircraft show a factor of about 14. >>></p>
<p><strong>Practical implications</strong> – The mass growth factor has been revisited in order to fully embrace the concept of mass growth and may lead to a better general understanding of aircraft design. >>></p>
<p><strong>Social implications</strong> – A detailed discussion of aircraft costs as well as aircraft development requires detailed knowledge of the aircraft. By understanding the mass growth factor, consumers can have this discussion with industry at eye level. >>></p>
<p><strong>Originality/value</strong> – The derivation of the equation for the direct calculation of the mass growth factor and the determination of the factor using the method for 90% of current passenger aircraft was not shown.</p>
http://EWADE.AircraftDesign.org --- http://Presentations2020.AircraftDesign.org
https://doi.org/10.5281/zenodo.4159259
oai:zenodo.org:4159259
eng
Zenodo
https://doi.org/10.7910/DVN/6NHDDP
https://zenodo.org/communities/profscholz
https://zenodo.org/communities/ewade
https://doi.org/10.5281/zenodo.4159258
info:eu-repo/semantics/openAccess
Creative Commons Attribution Non Commercial Share Alike 4.0 International
https://creativecommons.org/licenses/by-nc-sa/4.0/legalcode
EWADE/READ 2020, 15th European Workshop on Aircraft Design Education, Rzeszów, Poland / Online, 21.-22.10.2020
EWADE2020
aviation
aircraft
passenger
mass
growth
payload
range
fuel
consumption
aerodynamics
Prof. Scholz @ Zenodo
Understanding the Aircraft Mass Growth and Reduction Factor
info:eu-repo/semantics/lecture
oai:zenodo.org:546431
2020-01-20T13:17:30Z
openaire
user-ewade
Zafirov, Dimo
Panayotov, Hristian
2013-09-18
<p>UAV Activities in TU-Sofia (Branch Plovdiv): Joined wing investigations; UAVs; Ducted fans; Autonomous flights; Vertical takeoff and landing aircraft.</p>
http://EWADE.AircraftDesign.org --- http://ProceedingsEWADE2013.AircraftDesign.org
https://doi.org/10.5281/zenodo.546431
oai:zenodo.org:546431
Zenodo
https://zenodo.org/communities/ewade
https://doi.org/
info:eu-repo/semantics/openAccess
Creative Commons Attribution 4.0 International
https://creativecommons.org/licenses/by/4.0/legalcode
EWADE 2013, 11th European Workshop on Aircraft Design Education, Linköping, Sweden, 17.-19.09.2013
EWADE2013
aircraft
design
teaching
education
research
university
Europe
workshop
UAV Research and Development in Technical University Sofia
info:eu-repo/semantics/lecture
oai:zenodo.org:546427
2020-01-20T14:47:33Z
openaire
user-ewade
Sartorius, Sky
2013-09-18
<p>Design at TUM – a broad topic. Unique boundary conditions at TUM. Course content/curriculum/scope. Prescribed design methods and tools. Course development, (short) history, past years. Lessons learned. Future of aircraft design education at TUM.</p>
http://EWADE.AircraftDesign.org --- http://ProceedingsEWADE2013.AircraftDesign.org
https://doi.org/10.5281/zenodo.546427
oai:zenodo.org:546427
Zenodo
https://zenodo.org/communities/ewade
https://doi.org/
info:eu-repo/semantics/openAccess
Creative Commons Attribution 4.0 International
https://creativecommons.org/licenses/by/4.0/legalcode
EWADE 2013, 11th European Workshop on Aircraft Design Education, Linköping, Sweden, 17.-19.09.2013
EWADE2013
aircraft
design
teaching
education
research
university
Europe
workshop
The New Aircraft Design Course at the Technical University of Munich (TUM)
info:eu-repo/semantics/lecture
oai:zenodo.org:6038546
2022-02-11T01:49:27Z
openaire
user-ewade
Topolewski, Rafal
2020-10-21
<p>Distributed electric propulsion (DEP) enables to easily apply distributed propulsion to aircraft. DEP generates greater lifting forces but also greater drag forces. To achieve better aerodynamic characteristics, the wing geometry must be modified based on optimization.</p>
http://EWADE.AircraftDesign.org --- http://Presentations2020.AircraftDesign.org
https://doi.org/10.5281/zenodo.6038546
oai:zenodo.org:6038546
eng
Zenodo
https://zenodo.org/communities/ewade
https://doi.org/10.5281/zenodo.6038545
info:eu-repo/semantics/openAccess
Creative Commons Attribution 4.0 International
https://creativecommons.org/licenses/by/4.0/legalcode
EWADE/READ 2020, 15th European Workshop on Aircraft Design Education, Rzeszów, Poland / Online, 21.-22.10.2020
EWADE2020
Aircraft
Engine
Propeller
Aerodynamics
Leading Edge
Distributed Electric Propulsion
DEP
Vessel
Moving Deck
Leading Edge Distributed and Non-Distributed Electric Propulsion Comparison on a Moving Vessel Deck
info:eu-repo/semantics/lecture
oai:zenodo.org:546617
2020-10-08T17:13:16Z
openaire
user-ewade
user-profscholz
Scholz, Dieter
Sousa, Tahir
2013-09-18
<p>A 3D visualization is missing for many aircraft preliminary sizing tools. NASA’s Open Vehicle Sketch Pad (OpenVSP) is easy to use, but lacks an interface to input consistent aircraft data. Such an interface has been programmed and is called OpenVSP-Connect. Aircraft are sketched from about 50 parameters. If these are not known to the user, the interface calculates them as good as possible based on simple equations from aircraft design or statistics. Taken this to the extreme, a decent looking aircraft is drawn from as few as two or three input parameters.</p>
http://EWADE.AircraftDesign.org --- http://ProceedingsEWADE2013.AircraftDesign.org
https://doi.org/10.5281/zenodo.546617
oai:zenodo.org:546617
Zenodo
https://zenodo.org/communities/profscholz
https://zenodo.org/communities/ewade
https://doi.org/10.5281/zenodo.796593
info:eu-repo/semantics/openAccess
Creative Commons Attribution 4.0 International
https://creativecommons.org/licenses/by/4.0/legalcode
EWADE 2013, 11th European Workshop on Aircraft Design Education, Linköping, Sweden, 17.-19.09.2013
EWADE2013
aircraft
design
sizing
conceptual
open
sketch
interface
Excel
NASA
teaching
education
research
Europe
workshop
OpenVSP-Connect - Visualize Your Aircraft Sizing Results with NASA's Vehicle Sketch Pad
info:eu-repo/semantics/lecture
oai:zenodo.org:6038251
2022-02-11T01:49:31Z
openaire
user-ewade
Jungo, Aidan
Riolo, Vivien
Vos, Jan
2020-10-21
<p>CEASIOMpy is an open source conceptual aircraft design environment. CEASIOMpy can be used to set up complex design and optimization workflows, both for conventional and unconventional configurations. CEASIOMpy provides tools for various disciplines in aircraft design, amongst others: Geometry and meshes, weight and balance, aerodynamics, structures, mission analysis, stability analysis. CEASIOMpy uses the open-standard format CPACS. Workflows can be set up with the open-source environment RCE. Both CPACS and RCE are actively developed by the German Aerospace Center DLR. Follow the links below to learn how get started or how to contribute to the project. CEASIOMpy uses surrogate models to speed up the creation of aerodynamic databases.</p>
http://EWADE.AircraftDesign.org --- http://Presentations2020.AircraftDesign.org
https://doi.org/10.5281/zenodo.6038251
oai:zenodo.org:6038251
eng
Zenodo
https://zenodo.org/communities/ewade
https://doi.org/10.5281/zenodo.6038250
info:eu-repo/semantics/openAccess
Creative Commons Attribution 4.0 International
https://creativecommons.org/licenses/by/4.0/legalcode
EWADE/READ 2020, 15th European Workshop on Aircraft Design Education, Rzeszów, Poland / Online, 21.-22.10.2020
EWADE2020
CEASIOM
aerodynamics
Using Surrogate Models to Speed up the Creation of Aerodynamic Databases in CEASIOMpy
info:eu-repo/semantics/lecture
oai:zenodo.org:546657
2020-01-20T14:21:39Z
user-ewade
La Rocca, G.
Li, M.
Chiozzi, M.
2013-09-18
<p>This paper describes the conceptual study of a nuclear powered blended wing body aircraft for the cruiser/feeder concept. According to this radically new aviation paradigm, large transport aircraft (cruisers) carry passengers over long distances, while remaining airborne for very long periods. Smaller aircraft (feeders) take off from local airports, intercept the cruiser, dock and enable in-flight exchange of passengers and supplies. Preliminary studies indicated that cruiser concepts based on engines burning kerosene would be too heavy and feeders would need to operate also as tankers. Propelling the cruiser with a nuclear power source would yield very high efficiency parameters, even if the weight of the system would result higher due to the required reactor shielding. The blended wing body configuration was selected both for its potential advantages in terms of aerodynamic and structural efficiency, as well as for the use flexibility of its internal volume, necessary to integrate power plants and shielding, accommodate 1000 passengers and host the loading/unloading station for in-flight payload exchange. The daring nature of the proposed solution is compatible to the foreseen entry into service date, which is set for the last part of this century. The peculiar nature of the aircraft under consideration has required a somehow different conceptual design approach, than generally used for conventional passenger transport aircraft. Apart from the inherent complexity related to the design of such a novel and integrated configuration as a blended wing body, the typical design approach based on the use of simple performance equations and statistics to achieve a first estimation of the main weight contributors was of little use in this case. From one side, the fuel mass used to perform the mission is just negligible; from the other, a method was necessary to account for the weight of the radiation shielding, which is a significant contribution to the overall aircraft weight. Rather than in the numerical results of the sizing process, the value of the design work described in this paper should be found in the very design approach and the preliminary ideas for integrating the passenger docking system and the nuclear power plant.</p>
http://EWADE.AircraftDesign.org --- http://ProceedingsEWADE2013.AircraftDesign.org
https://doi.org/10.5281/zenodo.546657
oai:zenodo.org:546657
Zenodo
https://zenodo.org/communities/ewade
https://doi.org/
info:eu-repo/semantics/openAccess
Creative Commons Attribution 4.0 International
https://creativecommons.org/licenses/by/4.0/legalcode
EWADE 2013, CEAS 2013, 11th European Workshop on Aircraft Design Education --- 4th CEAS Air & Space Conference, Linköping, Sweden, 17.-19.09.2013
cruiser
feeder
blended wing body
nuclear propulsion
in-flight passenger exchange
aircraft
design
resarch
university
Europe
workshop
EWADE2013
CEAS2013
Feasibility Study of a Nuclear Powered Blended Wing Body Aircraft for the Cruiser/Feeder Concept
info:eu-repo/semantics/conferencePaper
oai:zenodo.org:21440
2020-01-20T14:57:37Z
openaire
user-ewade
Chiesa, Sergio
Di Meo, Giovanni
Fioriti, Marco
Fusaro, Roberta
2013-09-18
<p>Italian University and Research Ministry (MIUR) stated that all the research projects of the cluster must be designed as an “Educational Program” (about 10% of the total amount of every project). So, Tecnologie Innovative per Velivoli di Aviazione Generale di Nuova Generazi, Innovative General Aviation Technologies (TIVANO) will pay five grants for PhD Students that will work for three years on the Project both in Industry and at University. The tutor will be an academic of Politecnico di Torino (POLITO) and will guide three of the aforesaid PhD students in the team that will work on the described activities.</p>
http://EWADE.AircraftDesign.org --- http://ProceedingsEWADE2013.AircraftDesign.org
https://doi.org/10.5281/zenodo.21440
oai:zenodo.org:21440
Zenodo
https://zenodo.org/communities/ewade
https://doi.org/
info:eu-repo/semantics/openAccess
Creative Commons Attribution 4.0 International
https://creativecommons.org/licenses/by/4.0/legalcode
EWADE 2013, 11th European Workshop on Aircraft Design Education, Linköping, Sweden, 17.-19.09.2013
hybrid propulsion
general aviation
light aircraft
aircraft
EWADE2013
Contributions from Educational Activities to Researches About Hybrid Propulsion Opportunities for Light Aircraft
info:eu-repo/semantics/lecture
oai:zenodo.org:546608
2020-01-20T14:46:30Z
openaire
user-ewade
De Roo, R.
Verbeke, J.
Becuwe, I.
2013-09-18
<p>The Vives UAS competence centre: Successful start. More than 30 students, both national and international have been involved in UAS research and development. UAS course from Sept. 2013. In the future, the focus will lie on further expansion towards the industry and starting new projects together with other academia and companies.</p>
http://EWADE.AircraftDesign.org --- http://ProceedingsEWADE2013.AircraftDesign.org
https://doi.org/10.5281/zenodo.546608
oai:zenodo.org:546608
Zenodo
https://zenodo.org/communities/ewade
https://doi.org/
info:eu-repo/semantics/openAccess
Creative Commons Attribution 4.0 International
https://creativecommons.org/licenses/by/4.0/legalcode
EWADE 2013, 11th European Workshop on Aircraft Design Education, Linköping, Sweden, 17.-19.09.2013
EWADE2013
aircraft
design
teaching
education
research
university
Europe
workshop
Development of UAS for Scientific Monitoring
info:eu-repo/semantics/lecture
oai:zenodo.org:546414
2020-01-20T13:40:44Z
openaire
user-ewade
Nicolosi, F.
Della Vecchia, P.
Ciliberti, D.
2013-09-18
<p>A new procedure to evaluate the aerodynamic interference of airplane’s components on the vertical tailplane has been proposed. It has been developed by solving Navier-Stokes equations in a fully turbulent subsonic flow regime on more than 200 regional turboprop aircraft configurations, with the aim to bring CFD into aircraft preliminary design.</p>
http://EWADE.AircraftDesign.org --- http://ProceedingsEWADE2013.AircraftDesign.org
https://doi.org/10.5281/zenodo.546414
oai:zenodo.org:546414
Zenodo
https://zenodo.org/communities/ewade
https://doi.org/
info:eu-repo/semantics/openAccess
Creative Commons Attribution 4.0 International
https://creativecommons.org/licenses/by/4.0/legalcode
EWADE 2013, 11th European Workshop on Aircraft Design Education, Linköping, Sweden, 17.-19.09.2013
EWADE2013
aircraft
design
teaching
education
research
university
Europe
workshop
A New Vertical Tail Design Procedure for General Aviation and Turboprop Aircraft
info:eu-repo/semantics/lecture
oai:zenodo.org:18921
2020-10-08T17:22:12Z
openaire
user-ewade
user-profscholz
Scholz, Dieter
2013-09-18
<p>The first Open Access (OA) peer reviewed online journals in aerospace were all established after 2007. Still today more and more OA aerospace journals get started. Many publishers are located in less developed countries. The benefits of OA publishing are undisputed in the academic community, but there is disagreement if the new publishers can work to required standards. The current situation is evaluated based on an Internet review. OA journals in aerospace are listed with their major characteristics. Well know OA publishers charge high publication fees, whereas less known OA publishers tend to charge relatively low fees. All publishers need to be carefully checked for their level of rigor in peer review and their offered service in the scholarly publication process. Authors should evaluate OA journals and publishers against provided lists of criteria before submitting their work.</p>
http://EWADE.AircraftDesign.org --- http://ProceedingsEWADE2013.AircraftDesign.org
https://doi.org/10.5281/zenodo.18921
oai:zenodo.org:18921
Zenodo
https://zenodo.org/communities/profscholz
https://zenodo.org/communities/ewade
https://doi.org/
info:eu-repo/semantics/openAccess
Creative Commons Attribution 4.0 International
https://creativecommons.org/licenses/by/4.0/legalcode
EWADE 2013, 11th European Workshop on Aircraft Design Education, Linköping, Sweden, 17.-19.09.2013
Open Access
Self-Archiving
OAS
journal
aerospace
aeronautics
space
research
open
access
AAST
INCAS
criteria
business
model
EWADE2013
2013
Open Access Publishing in Aerospace – Opportunities and Pitfalls
info:eu-repo/semantics/lecture
oai:zenodo.org:546693
2020-01-20T13:40:17Z
user-ewade
Moerland, Erwin
Becker, Richard-Gregor
Nagel, Björn
2013-09-18
<p>Covering all relevant physical effects and mutual influences during aircraft preliminary design at a sufficient level of fidelity necessitates simultaneous consideration of a large number of disciplines. This requires an approach in which teams of engineers apply their analysis tools and knowledge to collaboratively approach design challenges. In the current work, recent technical advancements of the German Aerospace Center (DLR) in data and workflow management are utilized for establishing a toolbox containing elementary disciplinary analysis modules. This toolbox is focussed on providing fast overall aircraft design capabilities. The incorporated empirical and physics based tools of low fidelity level can be used for setting up modular design workflows, tailored for the design cases under consideration. This allows the involved engineers to identify initial design trends at a low computational effort. Furthermore, areas of common physical affinity are identified, serving as a basis for communication and for incorporating tools of higher fidelity in later phases of the design process. Clear visualisation methods aid in efficiently translating knowledge between the involved engineers within the identified areas of common affinity. A system-of-systems approach is stablished by applying the elementary aircraft design toolbox for the establishment of requirement catalogues for engine preliminary design. The engine designers at their turn deliver initial performance correlations for application in the aircraft design toolbox. In this way, a clear synergy is established between the design of both the airframe and power plant. Using this approach, engineers of different technical backgrounds share their knowledge in a collaborative design approach. The use case guiding the present work involves a conventional short to medium range aircraft sent at half the design range. The wing area and aspect ratio are varied to investigate the influence on the engine requirements catalogue for this particular mission.</p>
http://EWADE.AircraftDesign.org --- http://ProceedingsEWADE2013.AircraftDesign.org
https://doi.org/10.5281/zenodo.546693
oai:zenodo.org:546693
Zenodo
https://zenodo.org/communities/ewade
https://doi.org/
info:eu-repo/semantics/openAccess
Creative Commons Attribution 4.0 International
https://creativecommons.org/licenses/by/4.0/legalcode
EWADE 2013, CEAS 2013, 11th European Workshop on Aircraft Design Education --- 4th CEAS Air & Space Conference, Linköping, Sweden, 17.-19.09.2013
collaborative design
MDO
knowledge management
CPACS
RCE
aircraft
design
Europe
workshop
EWADE2013
CEAS2013
Collaborative Understanding of Disciplinary Correlations Using a Low-Fidelity Physics Based Aerospace Toolkit
info:eu-repo/semantics/conferencePaper
oai:zenodo.org:546482
2020-01-20T15:09:45Z
openaire
user-ewade
La Rocca, G.
Li, M.
Chiozzi, M.
2013-09-18
<p>In the RECREATE (REsearch on a CRuiser Enabled Air Transport Environment) project, European research institutes, universities<br>
and small businesses work together to investigate a future air transportation system based on the cruiser-feeder concept. Next to In Flight Refueling operations for passenger aircraft, the feasibility study of Nuclear Powered Blended Wing body aircraft for in flight exchange of payload is second concept addressed by RECREATE.</p>
http://EWADE.AircraftDesign.org --- http://ProceedingsEWADE2013.AircraftDesign.org
https://doi.org/10.5281/zenodo.546482
oai:zenodo.org:546482
Zenodo
https://zenodo.org/communities/ewade
https://doi.org/
info:eu-repo/semantics/openAccess
Creative Commons Attribution 4.0 International
https://creativecommons.org/licenses/by/4.0/legalcode
EWADE 2013, 11th European Workshop on Aircraft Design Education, Linköping, Sweden, 17.-19.09.2013
EWADE2013
aircraft
design
teaching
education
research
university
Europe
workshop
Feasibility Study of a Nuclear Powered Blended Wing Body Aircraft for the Cruiser/ Feeder Concept
info:eu-repo/semantics/lecture
oai:zenodo.org:6038456
2022-02-11T01:49:26Z
openaire
user-ewade
Krawczyk, Natalia
2020-10-21
<p>Thermal comfort is related to the feeling of well-being; of not feeling cold or hot. The Fanger model tries to predict this. Measurements have been made. There are significant differences between actual thermal sensations (from questionnaires) and the Fanger model. Thus, the best solution might be to modify the Fanger model.</p>
http://EWADE.AircraftDesign.org --- http://Presentations2020.AircraftDesign.org
https://doi.org/10.5281/zenodo.6038456
oai:zenodo.org:6038456
eng
Zenodo
https://zenodo.org/communities/ewade
https://doi.org/10.5281/zenodo.6038455
info:eu-repo/semantics/openAccess
Creative Commons Attribution 4.0 International
https://creativecommons.org/licenses/by/4.0/legalcode
EWADE/READ 2020, 15th European Workshop on Aircraft Design Education, Rzeszów, Poland / Online, 21.-22.10.2020
EWADE2020
aircraft
cabin
comfort
model
temperature
humidity
Analysis of Thermal Comfort on Planes
info:eu-repo/semantics/lecture
oai:zenodo.org:546420
2020-01-20T17:39:34Z
openaire
user-ewade
de Paula, Adson Agrico
2013-09-18
<p>The case study motivated strongly the engineering students students, since this activity established a relationship between theory and practice. The education goals were achieved (requirements, design philosophy and multidisciplinary view view).Teaching-learning process of Aeronautics is a great pedagogical opportunity. There are many possibilities applying case study in aeronautical education. Case Study fits well with wide ide engineering problem scenario training students to deal with different engineering situations.</p>
http://EWADE.AircraftDesign.org --- http://ProceedingsEWADE2013.AircraftDesign.org
https://doi.org/10.5281/zenodo.546420
oai:zenodo.org:546420
Zenodo
https://zenodo.org/communities/ewade
https://doi.org/
info:eu-repo/semantics/openAccess
Creative Commons Attribution 4.0 International
https://creativecommons.org/licenses/by/4.0/legalcode
EWADE 2013, 11th European Workshop on Aircraft Design Education, Linköping, Sweden, 17.-19.09.2013
EWADE2013
aircraft
design
teaching
education
research
university
Europe
workshop
A Case Study in Aeronautical Engineering Education
info:eu-repo/semantics/lecture