Accession Number : AD0848019

Title :   Model 8-82 Wing-Tip Deflection Test,

Corporate Author : GENERAL DYNAMICS SAN DIEGO CA CONVAIR DIV

Personal Author(s) : Haney, R. J. ; Wise, W. E.

Report Date : 03 JUN 1954

Pagination or Media Count : 48

Abstract : The report describes results obtained from applied loading of the wing surfaces of an F-102 aircraft.

Descriptors :   (*JET FIGHTERS, DELTA WINGS), (*DELTA WINGS, DEFLECTION), LOADS(FORCES), LOAD DISTRIBUTION, FORCE(MECHANICS), MODEL TESTS.

Subject Categories : Attack and Fighter Aircraft
      Mechanics

Distribution Statement : APPROVED FOR PUBLIC RELEASE