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[American Institute of Aeronautics and Astronautics 23rd AIAA Applied Aerodynamics Conference - Toronto, Ontario, Canada ()] 23rd AIAA Applied Aerodynamics Conference - Navier-Stokes Computations for a Grid Fin Missile

โœ Scribed by Ma, MingSheng; Deng, Youqi; Zheng, Ming; Zhou, Naichun


Book ID
121059674
Publisher
American Institute of Aeronautics and Astronautics
Year
2005
Weight
932 KB
Category
Article
ISBN
1624100589

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[American Institute of Aeronautics and A
โœ Ma, MingSheng; Deng, Youqi; Zheng, Ming; Zhou, Naichun ๐Ÿ“‚ Article ๐Ÿ“… 2005 ๐Ÿ› American Institute of Aeronautics and Astronautics โš– 932 KB

Viscous computational fluid dynamic simulations are used to predict the aerodynamic coefficients and flowfield for a missile with grid fins. A grid fin is an unconventional lifting and control surface that consists of an outer frame supporting an inner grid of intersecting planar surfaces of small c