Drag Predictions for Projectiles at Transonic and Supersonic Speeds
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Defense Technical Information Center
Cited by 9 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. Optimized Ristorcelli’s Compressibility Correction to the $$k-\upomega $$ SST Turbulence Model for Base Flow Analysis;International Journal of Aeronautical and Space Sciences;2023-06-06
2. Drag Reduction with Optimum Designing of a Base Bleed Projectile Using Computational Analysis;Innovations in Sustainable Energy and Cleaner Environment;2019-07-20
3. In-Pipe Aerodynamic Characteristics of a Projectile in Comparison with Free Flight for Transonic Mach Numbers Between 0.5 and 1.5;31st International Symposium on Shock Waves 2;2019
4. In-pipe aerodynamic characteristics of a projectile in comparison with free flight for transonic Mach numbers;Shock Waves;2018-03-21
5. Improvement of the Newtonian Method to Estimate Supersonic Vehicle Drag;Journal of Aerospace Engineering;2015-09
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