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Subsonic Flow CFD Investigation of Canard- Controlled Missile with Planar and Grid Fins

机译：平面和网格鳍片的Canard控制导弹的亚音速流CFD研究

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来源
《Aerospace Sciences Meeting and Exhibit》|2003年|1-13|共13页
会议地点 Reno, NV(US)
作者
J. DeSpirito; U.S; M. Vaughn; W. Washington; U.S;
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作者单位

. Army Research Laboratory Aberdeen Proving Ground MD;

. Army Aviation and Missile Command Redstone Arsenal AL;

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3. Planar Velocimetry of a Fin Trailing Vortex in Subsonic Compressible Flow [J] . Steven J. Beresh, John F. Henfling, Russell W. Spillers AIAA Journal . 2009,第7期

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4. Subsonic Flow CFD Investigation of Canard- Controlled Missile with Planar and Grid Fins [C] . Aerospace Sciences Meeting and Exhibit . 2003

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Subsonic Flow CFD Investigation of Canard- Controlled Missile with Planar and Grid Fins

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