Global Heat Transfer Measurement in a Hypersonic Shock Tunnel Using Temperature-Sensitive Paint

Author(s):  
Kazuyuki Nakakita ◽  
Tatsuya Osafune ◽  
Keisuke Asai
Author(s):  
M Saiprakash ◽  
C SenthilKumar ◽  
G Balu ◽  
V Shanmugam ◽  
Singh Prakash Rampratap ◽  
...  

In this article, experiments are carried out in a hypersonic shock tunnel with helium as driver gas and air as the test gas to obtain the convective heating rate and surface pressure distribution on a cone model placed at hypersonic speed. Test is performed in hypersonic shock tunnel for a flow Mach number of 6.5 at two different angles of attack, 0° and 5°. The sputtered thin film platinum sensors are used to measure the heat flux on a cone model. The measured heat-transfer rate compares well with theoretically estimated values using reference enthalpy method and computational fluid dynamics (CFD) simulation. The measured surface pressure compares well with CFD.


2018 ◽  
Vol 27 (4) ◽  
pp. 373-381
Author(s):  
Qiu Wang ◽  
Jiwei Li ◽  
Jinping Li ◽  
Wei Zhao ◽  
Zonglin Jiang

Sadhana ◽  
2006 ◽  
Vol 31 (5) ◽  
pp. 557-581 ◽  
Author(s):  
Niranjan Sahoo ◽  
S. Saravanan ◽  
G. Jagadeesh ◽  
K. P. J. Reddy

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