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- W258988253 abstract "Report presenting free-fall testing of the airplane configuration described in the title to evaluate certain new testing techniques for near sonic speeds. Results regarding the drag measurements and pressure data are provided. The data obtained from this test is also compared to free-fall tests in the high-speed tunnel and for a rocket-powered free-flight model, and the results show generally satisfactory agreement." @default.
- W258988253 created "2016-06-24" @default.
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- W258988253 date "1952-04-08" @default.
- W258988253 modified "2023-09-24" @default.
- W258988253 title "Transonic Drag Characteristics and Pressure Distribution on the Body of a Wing-body Combination Consisting of a Body of Revolution of Fineness Ratio 12 and a Wing Having Sweepback of 45 Degrees, Aspect Ratio 4, Taper Ratio 0.6, and NACA 65A006 Airfoi" @default.
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