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[American Institute of Aeronautics and Astronautics 10th Atmospheric Flight Mechanics Conference - Gatlinburg,TN,U.S.A. (15 August 1983 - 17 August 1983)] 10th Atmospheric Flight Mechanics Conference - Experimental investigation of rolling moment for a body-wing-tail missile configuration with wrap around wings and straight tails at supersonic speeds

✍ Scribed by WASHINGTON, W.

Book ID: 121030000
Publisher: American Institute of Aeronautics and Astronautics
Year: 1983
Weight: 382 KB
Category: Article
DOI: 10.2514/6.1983-2081

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