First program concerns airframe vibratory loads encountered during flight tests of VZ-2 tilt-wing VTOL aircraft throughout operational range from hover to cruise flight; wing stall and tail buffeting in descents were primary sources of airframe vibrations; second program concerns initial results of structural loads survey conducted as wind tunnel test and deals with steady wing loads measured throughout simulated transition from hover to cruise.
Structural-loads surveys on two tilt-wing VTOL configurations
NASA -- Tech Note
1961
13 pages
Article (Journal)
English
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WING TILT SCHEDULING IN TANDEM-WING VTOL CONFIGURATIONS
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