Effectiveness of Aerospike for Drag Reduction on a Blunt Cone in Hypersonic Flow

Vinayak N. Kulkarni; Viren I. Menezes; K. P. J. Reddy

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Effectiveness of Aerospike for Drag Reduction on a Blunt Cone in Hypersonic Flow

机译：Aerospike在高超音速流钝锥上减阻的有效性

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来源
《Journal of Spacecraft and Rockets》 |2010年第3期|p.542-544|共3页
作者
Vinayak N. Kulkarni; Viren I. Menezes; K. P. J. Reddy;
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作者单位

Vinayak KulkarniIndian Institute of Technology Guwahati,Guwahati, 781 039, IndiaViren Menezes∗Indian Institute of Technology Bombay,Mumbai, 400 076, IndiaandK. P. J. ReddyIndian Institute of Science, Bangalore, 560 012, India;

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收录信息美国《科学引文索引》(SCI);美国《工程索引》(EI);
原文格式 PDF
正文语种 eng
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1. 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
2. Drag Reduction Optimization for Hypersonic Blunt Body with Aerospikes [J] . Wan T, Liu CM Journal of Aeronautics & Aerospace Engineering . 2017,第4期

机译：带有气钉的高超声速钝体的减阻优化
3. 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
4. Aerodynamic Drag Reduction Using Aerospikes for Large Angle Blunt Cone Flying at Hypersonic Mach Number [C] . V. Menezes, S. Saravanan, G. Jagadeesh, AIAA Fluid Dynamics Conference and Exhibit . 2002

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
5. Viscous optimized hypersonic waveriders designed from flows over cones and minimum drag bodies. [D] . Corda, Stephen. 1988

机译：粘性优化的高超声速行波器是根据锥和最小阻力体上的流动设计的。
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. Hypersonic Flow Field Reconfiguration and Drag Reduction of Blunt Body with Spikes and Sideward Jets [O] . Guilai Han, Zonglin Jiang 2018

机译：高超声速流场重新配置，用尖峰和向侧喷射拖曳钝器的减少
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

Effectiveness of Aerospike for Drag Reduction on a Blunt Cone in Hypersonic Flow

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