Aircraft Parameter / Performance Estimation from Flight Test and Dynamic Wind Tunnel Tests | India Science, Technology & Innovation - ISTI Portal

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

Implementing Organization

National Research Development Corporation (NRDC), New Delhi

About

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.

Related Innovations

Quick Information

Area of Research

Engineering Sciences

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