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What is Canard Missile Stability and Control Analysis about?
A flight investigation was conducted to determine the longitudinal stability and control characteristics of a 60-degree delta wing canard missile configuration. Results showed that the longitudinal stability derivatives had no unusual trends and varied gradually with Mach number between 0.7 to 1.45. Control effectiveness was maintained throughout the Mach number range, though lift produced by control surfaces was slightly positive at subsonic speeds and slightly negative at supersonic speeds. Hinge moments
- Author
- Iman Saberi
- Language
- EN