This publication contains three papers presented to the Aeroelasticity Sub-Committee of the AGARD Structures and Materials Panel at its 60th Meeting. The papers show that static aeroelasticity is increasingly being considered as a primary design parameter, affecting as it does structural optimisation, vehicle aerodynamic stability control effectiveness and overall performance.
Static Aeroelasticity in Combat Aircraft
1986
44 pages
Report
No indication
English
Static aeroelasticity in combat aircraft
TIBKAT | 1986
|Static Aeroelasticity and Flutter
Wiley | 2014
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