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NASA NTRS · 19630012385

A CALCULATION METHOD FOR SOLVING AEROELASTIC PROBLEMS FOR STUB WINGS AND ENTIRE AIRCRAFT

Kussner, H. G.
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Abstract

Calculation method for solving aeroelastic problems for stub wings and entire aircraft

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AIRCRAFT DESIGNWINGAEROELASTICITY

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BibTeXRIS

Kussner, H. G.. 1963-09-01. A CALCULATION METHOD FOR SOLVING AEROELASTIC PROBLEMS FOR STUB WINGS AND ENTIRE AIRCRAFT. https://ntrs.nasa.gov/citations/19630012385

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