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- W4238328591 abstract "The main factors determining the shape of a supersonic aeroplane or missile are aerodynamic in origin. However, as always, a compromise with structural considerations must be achieved, zero wing thickness for supersonic aircraft being just as unattainable as infinite aspect ratio for subsonic ones. This compromise is more far-reaching in the supersonic aircraft because of the much greater importance of aeroelasticity. In addition, there are entirely new problems which arise from the high structural temperatures attained in supersonic flight." @default.
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- W4238328591 date "1956-11-01" @default.
- W4238328591 modified "2023-09-30" @default.
- W4238328591 title "Structures" @default.
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- W4238328591 doi "https://doi.org/10.1017/s0001924000127769" @default.
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