Accession Number : AD0370569

Title :   Z(XQ-5)ZTEST WING VIBRATION TEST.

Corporate Author : LOCKHEED AIRCRAFT CORP VAN NUYS CALIF

Personal Author(s) : Lien,A. T.

Report Date : 11 JAN 1956

Pagination or Media Count : 44

Abstract : An XQ-5 test wing mounted in a supporting fixture, was subjected to vibratory excitations of 10 to 150 cps to determine resonant frequencies, relative amplitudes, node line locations and damping coefficients. The test yielded reasonably satisfactory data which enabled accomplishment of its purpose. (Author)

Descriptors :   (*TARGET DRONES, WINGS), TEST METHODS, VIBRATION, DESIGN, PERFORMANCE(ENGINEERING), DRONES, AERIAL TARGETS (U) AMPLITUDE MODULATION, RESONANCE, DAMPING, BENDING, SUPERSONIC TEST VEHICLES

Subject Categories : Pilotless Aircraft
      Research and Experimental Aircraft
      Fluid Mechanics
      Unmanned Spacecraft

Distribution Statement : APPROVED FOR PUBLIC RELEASE