Accession Number : AD0028961


Title :   COMPARISON OF EXPERIMENTAL WITH CALCULATED RESULTS FOR THE LIFTING EFFECTIVENESS OF A FLEXIBLE 45 DEG SWEPTBACK WING OF ASPECT RATIO 6.0 AT MACH NUMBERS FROM 0.8 TO 1.3


Descriptive Note : Research memo.


Corporate Author : NATIONAL AERONAUTICS AND SPACE ADMIN LANGLEY RESEARCH CENTER HAMPTON VA


Personal Author(s) : WALTERS, RICHARD E


Full Text : https://apps.dtic.mil/dtic/tr/fulltext/u2/028961.pdf


Report Date : 15 Apr 1954


Pagination or Media Count : 40


Descriptors :   *AERODYNAMIC CHARACTERISTICS , *SWEPTBACK WINGS , LIFT


Subject Categories : Aircraft
      Fluid Mechanics


Distribution Statement : APPROVED FOR PUBLIC RELEASE