Compilation of 7 papers presented at symposium; first section of lectures deals with theoretical methods for demonstrating resistance to flutter of aircraft; second section covers experimental procedures for obtaining parameters for calculation of flutter, including wind-tunnel measurement of aerodynamic forces on vibrating wings, measurements in electropotential tank as means of analogy in determination of theoretical aerodynamic forces, and static vibration test on actual aircraft as means for determination of elastic and mass parameters.
Aeroelasticity Symposium -- Goettingen, April 16-17, 1957
NASA -- Tech Translation
1963
192 pages
Article (Journal)
English
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Aeroelasticity Symposium, Göttingen, April 16 - 17, 1957
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