External fuel tanks or missiles degrade stability because of unsteady aerodynamics. Transonic aeroelasticity of wings with tip stores simulated with improved version of ATRAN3S computer code, previously used to study behavior of clean wings only. Output of code agrees well with wind-tunnel data.
Aeroelastic Computations For Wings With Loaded Tips
NASA Tech Briefs ; 12 , 4
01.04.1988
Sonstige
Keine Angabe
Englisch
British Library Conference Proceedings | 1994
|Predicted static aeroelastic effects on wings with supersonic leading edges and streamwise tips
Engineering Index Backfile | 1959
|