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- W926972144 abstract "A method of computing the power spectral densities of the lateral response of airplanes to random atmospheric turbulence was adapted to an electronic digital computer. By use of this program, the power spectral densities of the lateral roll, yaw, and sideslip angular displacement of several conventional and STOL airplanes were computed. The results show that for the conventional airplanes, the roll response is more prominent than that for yaw or sideslip response. For the STOL airplanes, on the other hand, the yaw and sideslip responses were larger than the roll response. The response frequency of the STOL airplanes generally is higher than that for the conventional airplanes. This combination of greater sensitivity of the STOL airplanes in yaw and sideslip and the frequency at which they occur could be a factor causing the poor riding qualities of this class of airplanes." @default.
- W926972144 created "2016-06-24" @default.
- W926972144 creator A5007749983 @default.
- W926972144 date "1974-03-01" @default.
- W926972144 modified "2023-09-26" @default.
- W926972144 title "Computed lateral power spectral density response of conventional and STOL airplanes to random atmospheric turbulence" @default.
- W926972144 hasPublicationYear "1974" @default.
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