[American Institute of Aeronautics and Astronautics 23rd AIAA Applied Aerodynamics Conference - Toronto, Ontario, Canada ()] 23rd AIAA Applied Aerodynamics Conference - Numerical Investigation on the Leeside Vortex Manipulation of a Generic Missile

[American Institute of Aeronautics and A

[American Institute of Aeronautics and Astronautics 23rd AIAA Applied Aerodynamics Conference - Toronto, Ontario, Canada ()] 23rd AIAA Applied Aerodynamics Conference - Vortex Filament Simulation of Trailing Vortex Merger

✍ Anand, Gaurav; Graham, Will 📂 Article 📅 2005 🏛 American Institute of Aeronautics and Astronautics ⚖ 491 KB

[American Institute of Aeronautics and A

[American Institute of Aeronautics and Astronautics 23rd AIAA Applied Aerodynamics Conference - Toronto, Ontario, Canada ()] 23rd AIAA Applied Aerodynamics Conference - A Cambered Body Method for Missile Datcom

✍ Blake, William; Karni, Etan 📂 Article 📅 2005 🏛 American Institute of Aeronautics and Astronautics ⚖ 205 KB

[American Institute of Aeronautics and A

[American Institute of Aeronautics and Astronautics 23rd AIAA Applied Aerodynamics Conference - Toronto, Ontario, Canada ()] 23rd AIAA Applied Aerodynamics Conference - High Angle of Attack Aerodynamic Predictions Using Missile Datcom

✍ Abney, Eric; McDaniel, Melissa 📂 Article 📅 2005 🏛 American Institute of Aeronautics and Astronautics ⚖ 244 KB

[American Institute of Aeronautics and A

[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

✍ Ma, MingSheng; Deng, Youqi; Zheng, Ming; Zhou, Naichun 📂 Article 📅 2005 🏛 American Institute of Aeronautics and Astronautics ⚖ 932 KB

[American Institute of Aeronautics and A

[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

✍ Ma, MingSheng; Deng, Youqi; Zheng, Ming; Zhou, Naichun 📂 Article 📅 2005 🏛 American Institute of Aeronautics and Astronautics ⚖ 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

[American Institute of Aeronautics and A

[American Institute of Aeronautics and Astronautics 23rd AIAA Applied Aerodynamics Conference - Toronto, Ontario, Canada ()] 23rd AIAA Applied Aerodynamics Conference - Aerodynamic Performance Study of Flapping-Wing Flowfields

✍ Lin, San-Yih; Hu, Jeu-Jiun 📂 Article 📅 2005 🏛 American Institute of Aeronautics and Astronautics ⚖ 480 KB