ELECTRICAL DISCHARGE TECHNIQUE FOR THREE-DIMENSIONAL FLOW FIELD VISUALIZATION IN HYPERSONIC SHOCK TUNNEL

Author:

Jagadeesh G.,Rao B. R. Srinivasa,Nagashetty K.,Reddy N. M.,Reddy K. P. J.

Publisher

Begell House

Subject

Computer Science Applications,Mechanical Engineering,Condensed Matter Physics

Cited by 6 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. Influence of shock waves from plasma actuators on transonic and supersonic airflow;Journal of Physics D: Applied Physics;2018-02-15

2. Shock Tunnels and Hypersonic Research in IISc, Bangalore;Experimental Methods of Shock Wave Research;2015-11-01

3. Experimental Investigations of Hypersonic Flow over Highly Blunted Cones with Aerospikes;AIAA Journal;2003-10

4. Aerodynamic Drag Reduction Using Aerospikes for Large Angle Blunt Cone Flying at Hypersonic Mach Number;22nd AIAA Aerodynamic Measurement Technology and Ground Testing Conference;2002-06-24

5. Studies on the Effects of Test Gas on the Flow Field around Large Angle Blunt Cone Flying at Hypersonic Mach Number.;TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES;2002

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