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- W607323346 abstract "Report presenting testing of a configuration with a body of fineness ratio 16.6, an unswept horizontal tail of aspect ratio 2.7, and a highly swept vertical tail, which were aeropulsed continuously in pitch during free flight with and without a sustainer rocket motor operating. Results regarding the pitching response, cross coupling, sustainer motor, angle of attack at zero normal force and tail flip, model aerodynamic center, induced jet effect are provided." @default.
- W607323346 created "2016-06-24" @default.
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- W607323346 date "1954-04-15" @default.
- W607323346 modified "2023-09-27" @default.
- W607323346 title "Rocket-powered model investigation of lift, drag, and stability of a body-tail configuration at Mach numbers from 0.8 to 2.3 and angles of attack between plus or minus 6.5 degrees" @default.
- W607323346 hasPublicationYear "1954" @default.
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