The Free Flight Aerodynamics Range
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Defense Technical Information Center
Cited by 8 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. Combining experimental data, computational fluid dynamics, and six-degree of freedom simulation to develop a guidance actuator for a supersonic projectile;Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering;2009-01-06
2. Effect of Spin Variation on Predicting the Dynamic Stability of Small-Caliber Ammunition;47th AIAA Aerospace Sciences Meeting including The New Horizons Forum and Aerospace Exposition;2009-01-05
3. Integration of Actuator Performance for Guiding Supersonic Projectiles;Journal of Spacecraft and Rockets;2008-05
4. Experimental Determination of the Effect of Rifling Grooves on the Aerodynamics of Small Caliber Projectiles;AIAA Atmospheric Flight Mechanics Conference and Exhibit;2006-06-25
5. Comparison of Predicted Actuator Performance for Guidance of Supersonic Projectiles to Measured Range Data;22nd Applied Aerodynamics Conference and Exhibit;2004-06-20
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