NASA NTRS · 19880000251
Aeroelastic Computations For Wings With Loaded Tips
Abstract
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.
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Goorjian, Peter M., Tu, Eugene L., Guruswamy, Guru P.. 1988-04-01. Aeroelastic Computations For Wings With Loaded Tips. https://ntrs.nasa.gov/citations/19880000251
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