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- W3045525321 abstract "An advanced rotation-balance apparatus has been developed for the Ames 12-ft pressure tunnel to study the effects of spin rate, angles of attack and sideslip, and, particularly, Reynolds number on the aerodynamics of fighter and general aviation aircraft in a steady spin. Angles of attack to 100 deg and angles of sideslip to 30 deg are possible with spin rates to 42 rad/sec (400 rpm) and Reynolds numbers to 30 million/m on fighter models with wing spans that are typically 0.7 m. A complete description of the new rotation-balance apparatus, the sting/balance/model assembly, and the operational capabilities is given." @default.
- W3045525321 created "2020-08-03" @default.
- W3045525321 creator A5019755536 @default.
- W3045525321 date "1978-04-19" @default.
- W3045525321 modified "2023-09-27" @default.
- W3045525321 title "New rotation-balance apparatus for measuring airplane spin aerodynamics in the wind tunnel" @default.
- W3045525321 doi "https://doi.org/10.2514/6.1978-835" @default.
- W3045525321 hasPublicationYear "1978" @default.
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