The project focuses on the development and testing of a strain gauge-based transducer to measure wall shear force on hypersonic models in short duration hypersonic test facilities. The transducer will be tested in a shock tunnel on a wedge model at Mach 8.46, and the results of skin friction parameters will be compared with the predicted values. The development will present a reliable, high-speed, stress measurement technique.
Outcome / Output
The project being undertaken by ISRO in collaboration with academia is directly or indirectly beneficial to the society.
Indian Space Research Organisation Headquarters (ISRO HQ)
Quick Information
Area of Research
Astronomy & Space Sciences
Focus Area
Hypersonic Aerodynamics
Status
Under Development
Output
No. of Research Paper
00
Technologies (If Any)
00
No. of PhD Produced
00
No. of Patents
Filed :00
Grant :00
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