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Skin friction measurement in hypersonic flows

Implementing Organization

Indian Institute of Technology Goa
Indian Institute of Technology (IIT)

About

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.
Funding Organization
Funding Organization
Indian Space Research Organisation Headquarters (ISRO HQ)
Quick Information
Thrust Areas
Astronomy & Space Sciences
Focus Area
Hypersonic Aerodynamics
Status
Under Development
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