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Shock Tunnel Studies of the Hypersonic Flowfield around the Hypervelocity Ballistic Models with Aerospikes

机译：带有气钉的超高速弹道模型周围高超音速流场的冲击隧道研究

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Experiments were carried out to investigate the effectiveness of a spike as a drag reduction tool for Hypervelocity Ballistic Model-1. Reduction in drag is observed when a spike is attached to the stagnation point of the model. Heat transfer studies are underway. Experiments are also planned in the shock tunnel to investigate the unsteady phenomena that occur with the spiked bodies.

机译：进行了实验，以研究尖峰钉作为超高速弹道模型1的减阻工具的有效性。当尖峰附着到模型的停滞点时，可以观察到阻力减小。传热研究正在进行中。还计划在冲击隧道中进行实验，以调查尖刺物体发生的不稳定现象。

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《International Symposium on Shock Waves》|2015年|681-685|共5页
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G. Balakalyani; S. Saravanan; G. Jagadeesh;
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Shock Tunnel Studies of the Hypersonic Flowfield around the Hypervelocity Ballistic Models with Aerospikes

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