Accession Number : AD0006725


Title :   EFFECT OF LEADING-EDGE CHORD-EXTENSIONS ON THE AERODYNAMIC CHARACTERISTICS OF A 45 SWEPTBACK WING-FUSELAGE COMBINATION AT MACH NUMBERS OF 0.40 TO 1.03


Descriptive Note : Reseach memo.


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


Personal Author(s) : West, Jr , F E ; Liner, George ; Martz, Gladys S


Full Text : https://apps.dtic.mil/dtic/tr/fulltext/u2/006725.pdf


Report Date : 14 Apr 1953


Pagination or Media Count : 43


Descriptors :   *FUSELAGES , *SWEPTBACK WINGS , LEADING EDGES , STABILITY , AERODYNAMIC CHARACTERISTICS


Subject Categories : Aircraft


Distribution Statement : APPROVED FOR PUBLIC RELEASE