Development program for acoustically loaded structure for DC-8 jet transport at Douglas Aircraft Co, using high-intensity-siren test facility and 24-in. sq panels; acoustic loads on structure determined by extrapolation of near field noise data of engines comparable in thrust to those of DC-8; relationships among load, response, and fatigue for both jet and sinusoidal loading investigated theoretically.
Development of aircraft structure to withstand acoustic loads
Aero/Space Eng
Aero/Space Engineering ; 18 , n 6
1959
7 pages
Aufsatz (Zeitschrift)
Englisch
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