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Bodies having Minimum Pressure Drag in Supersonic Flow- Investigating Nonlinear Effects

机译：在超音速流动中具有最小压力阻力的物体 - 研究非线性效应

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Antony Jameson;
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年度 2008
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1. Bodies Having Minimum Pressure Drag in Supersonic Flow: Investigating Nonlinear Effects [J] . Karthik Palaniappan, Antony Jameson Journal of Aircraft . 2010,第4期

机译：超声流中具有最小压力阻力的机构：研究非线性效应
2. Bodies Having Minimum Pressure Drag in Supersonic Flow: Investigating Nonlinear Effects [J] . Karthik Palaniappan, Antony Jameson Journal of Aircraft . 2010,第4期

机译：超声流中具有最小压力阻力的机构：研究非线性效应
3. Optimal Forebody Shape for Minimum Drag in Supersonic Flow [J] . G. Natarajan, N. Sahoo, V. Kulkarni Journal of The institution of engineers (India), Series C . 2015,第1期

机译：最佳前体形状，在超音速流中具有最小的阻力
4. Bodies Having Minimum Pressure Drag in Supersonic Flow: Investigating Nonlinear Effects [C] . K. Palaniappan, A. Jameson AIAA Guidance, Navigation, and Control Conference;Applied Aerodynamics Conference and Exhibit;AIAA/AAS Astrodynamics Specialist Conference and Exhibit . 2004

机译：超声流中具有最小压力阻力的机构：研究非线性效应
5. Experimental study on the effects of nose geometry on drag over axisymmetric bodies in supersonic flow. [D] . Brooker, B. Tyler. 2014

机译：鼻子几何形状对超声速流中轴对称物体上阻力的影响的实验研究。
6. Investigation of the Effects of Length to Depth Ratio on Open Supersonic Cavities Using CFD and Proper Orthogonal Decomposition [O] . Ibrahim Yilmaz, Ece Ayli, Selin Aradag 2013

机译：使用CFD和适当的正交分解研究长深比对开放超声腔的影响
7. An Analysis of Bodies Having Minimum Pressure Drag in Supersonic Flow: Exploring the Nonlinear Domain [O] . Antony Jameson 2014

机译：超音速流中具有最小压力阻力的体分析 - 非线性域探讨
8. INVESTIGATION OF MINIMUM DRAG AND MAXIMUM LIFT-DRAG RATIOS OF SEVERAL WING-BODY COMBINATIONS INCLUDING A CAMBERED TRIANGULAR WING AT LOW REYNOLDS NUMBERS AND AT SUPERSONIC SPEEDS [R] . Clinton E. Brown, L. K. Hargrave 1958

机译：低雷诺数和超速速下包括三角翼的几个翼体组合的最小拖曳和最大升降比的研究

Bodies having Minimum Pressure Drag in Supersonic Flow- Investigating Nonlinear Effects

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