The 2009 Version of the Aeroprediction Code: The AP09
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Cited by 5 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献
1. An Improved Method to Calculate the Nonlinear Rolling Moment Due to Differential Fin Deflection of Canard Controlled Missiles;AIAA Atmospheric Flight Mechanics Conference;2015-01-02
2. Computational Investigation of Pitch Damping on Missile Geometries at High Angles of Attack;30th AIAA Applied Aerodynamics Conference;2012-06-25
3. Approximate Method to Calculate Nonlinear Rolling Moment due to Differential Fin Deflection;Journal of Spacecraft and Rockets;2012-03
4. Improvements to Power-on Base Pressure Prediction for the Aeroprediction Code;Journal of Spacecraft and Rockets;2010-01
5. 2009 Version of the Aeroprediction Code: AP09;Journal of Spacecraft and Rockets;2008-07
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