Time-Accurate Numerical Prediction of Free Flight Aerodynamics of a Finned Projectile-Reference-Cited by-同舟云学术

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Time-Accurate Numerical Prediction of Free Flight Aerodynamics of a Finned Projectile

Published:2005-09-01 Issue: Volume: Page:
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Author:

Sahu Jubaraj

Publisher

Defense Technical Information Center

Cited by 17 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. Development of a Modularized Virtual Flight Simulator based on Multiple Discipline Coupled Method;Journal of Physics: Conference Series;2021-09-01

2. Application of a Coupling of Flight Mechanics and Aerodynamics to Predict the SHEFEX I Ascent Phase;Notes on Numerical Fluid Mechanics and Multidisciplinary Design;2013

3. Virtual Fly-Out Simulations of a Spinning Projectile from Subsonic to Supersonic Speeds;29th AIAA Applied Aerodynamics Conference;2011-06-27

4. Unsteady Aerodynamic Simulations of a Canard-Controlled Projectile at Low Transonic Speeds;AIAA Atmospheric Flight Mechanics Conference;2011-06-14

5. Estimation of Projectile Aerodynamic Coefficients Using Coupled CFD/RBD Simulation Results;AIAA Atmospheric Flight Mechanics Conference;2010-06-14

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