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Aerodynamic Drag Reduction Using Aerospikes for Large Angle Blunt Cone Flying at Hypersonic Mach Number

机译：使用气钉降低空气阻力，以高超声速马赫数飞行大角度钝锥

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《AIAA Fluid Dynamics Conference and Exhibit》|2002年|P.1-11|共11页
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V. Menezes; S. Saravanan; G. Jagadeesh; K. Reddy;
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中图分类流体动力学;
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1. Aerodynamic drag reduction by heat addition into the shock layer for a large angle blunt cone in hypersonic flow [J] . Kulkarni V, Hegde GM, Jagadeesh G, Physics of fluids . 2008,第8期

机译：通过在冲击层中增加热量来降低高超声速流动中大角度钝锥的气动阻力
2. Effectiveness of Aerospike for Drag Reduction on a Blunt Cone in Hypersonic Flow [J] . Vinayak N. Kulkarni, Viren I. Menezes, K. P. J. Reddy Journal of Spacecraft and Rockets . 2010,第3期

机译：Aerospike在高超音速流钝锥上减阻的有效性
3. Effectiveness of Aerospike for Drag Reduction on a Blunt Cone in Hypersonic Flow [J] . Vinayak Kulkarni, Viren Menezes, K. P. J. Reddy Journal of Spacecraft and Rockets . 2010,第3期

机译：Aerospike在高超音速流钝锥上减阻的有效性
4. Aerodynamic Drag Reduction Using Aerospikes for Large Angle Blunt Cone Flying at Hypersonic Mach Number [C] . American Institute of Aeronautics and Astronautics Fluid Dynamics Conference and Exhibit . 2002

机译：空气动力阻力减少使用Aerospikes用于大角度钝锥在超声波马赫数飞行
5. Hypersonic boundary-layer transition measurements at Mach 10 on a large seven-degree cone at angle of attack [D] . Moraru, Ciprian G. 2015

机译：在大七度锥面的迎角处以10马赫的高超声速边界层跃迁测量
6. Effect of a Roughness Element on the Receptivity of a Hypersonic Boundary Layer over a Blunt Cone Due to Pulse Entropy Disturbance with a Single Frequency [O] . Zhenqing Wang, Mingfang Shi, Xiaojun Tang, 2018

机译：粗糙元件对钝锥体上超声边界层的接受性的影响由于单频脉冲熵干扰
7. Studies on the Effects of Test Gas on the Flow Field around Large Angle Blunt Cone Flying at Hypersonic Mach Number. [O] . Gopalan Jagadeesh, Kanderpallt Nagashetty, K. P. Jaganntha Reddy, 2002

机译：超声波马赫数大角度钝锥围绕流域试验气体对流场影响的研究。
8. EXPERIMENTAL DETERMINATION OF AERODYNAMIC DRAG ON A BLUNTED 10-DEG CONE AT ANGLES OF ATTACK IN HYPERSONIC, RAREFIED FLOW [R] . David E. Boylan, William H. Sims 1964

机译：在超音速，稀有流动中攻击角度的10°锥形空气动力学实验测定

Aerodynamic Drag Reduction Using Aerospikes for Large Angle Blunt Cone Flying at Hypersonic Mach Number

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