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- W2156576627 abstract "A matrix method is presented for calculating the rigid and induced airload distribution for low aspect ratio wings with supersonic leading and trailing edges and inwardly raked tips. This method is applied to the static aeroelastic analysis of a set of missile fins for which experimental data is available for both the rigid and flexible cases. Comparisons are given between the theoretical and experimental values for several aerodynamic coefficients. Good agreement is shown in all cases for which data is available. The general construction of the matrices used in the aeroelastic analysis is also presented." @default.
- W2156576627 created "2016-06-24" @default.
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- W2156576627 date "1964-07-01" @default.
- W2156576627 modified "2023-09-27" @default.
- W2156576627 title "Aerodynamic matrix procedure for low aspect ratio wings" @default.
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- W2156576627 doi "https://doi.org/10.2514/3.43583" @default.
- W2156576627 hasPublicationYear "1964" @default.
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