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- W2110290445 abstract "This paper presents a discussion of an aircraft shaping method to control sonic boom overpressure levels along with the analysis of wind tunnel data which validated the method. The results indicate that the sonic boom minimization method can guide the design team choices of aircraft planform and component arrangement toward a low-boom-level configuration while permitting sufficient freedom and flexibility to satisfy other design criteria. Further, it is shown that off-design flight conditions do not drastically change the overpressure sonic boom shape and strength." @default.
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- W2110290445 date "1980-03-01" @default.
- W2110290445 modified "2023-09-27" @default.
- W2110290445 title "Some Effects of Applying Sonic Boom Minimization to Supersonic Cruise Aircraft Design" @default.
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- W2110290445 doi "https://doi.org/10.2514/3.57890" @default.
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