Review of current structural design criteria, analysis methods, and data handling techniques is presented, summarizing practices that result in large discrepancies between design loadings and those that occur in flight; alternate criteria, methods, or research are suggested which eliminate these discrepancies; emphasis is on methods of providing structural integrity for flight in stall buffet regime, and rational method is derived for predicting empennage loads at stall; design loadings resulting from application of method are compared with loads measured during flight tests of large, swept-wing, high subsonic transport.
Relationship between aircraft design and flight-measured loads
J Aircarft
Journal of Aircraft ; 4 , n 5
1967
7 pages
Aufsatz (Zeitschrift)
Englisch
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Analysis of Measured In-Flight Tail Loads
British Library Online Contents | 1996
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