Industrial Innovations

Aircraft Parameter / Performance Estimation from Flight Test and Dynamic Wind Tunnel Tests

I. For the first time in India planned aircraft flight-testing to estimate aerodynamic stability / control / performance data. II. For the first time a novel technique devised to derive stability control derivatives from wind tunnel tests in scaled models.

Area: Engineering Sciences

Funding agency: Department of Science and Technology (DST), Govt. of India

Implementing institute: National Research Development Corporation (NRDC), Govt. of India

Related links