Published May 31, 2019 | Version v1
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Optimization of Flight Time for Innovative Rotorcraft Designs through Advanced Experimental Techniques

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This paper presents a systematic approach to optimizing the flight time of rotorcraft designs, specifically focusing on autogyros. By employing the Design of Experiments (DoE) methodology alongside a rigorous Define, Measure, Analyze, Improve, Control (DMAIC) framework, we identify critical design parameters that significantly impact flight performance. Utilizing fractional factorial experiments and response surface methodology, we elucidate the relationship between design variables and flight time, aiming to exceed a target of 350 centi-seconds. The research underscores the importance of a robust measurement system, validated through Gage R&R analysis, and the application of advanced statistical tools for optimization.

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References

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