Accession Number : AD0093275


Title :   FLIGHT INVESTIGATION OF THE EFFECT OF A PROPULSIVE JET POSITIONED ACCORDING TO THE TRANSONIC AREA RULE ON THE DRAG COEFFICIENTS OF A SINGLE-ENGINE DELTA-WING CONFIGURATION AT MACH NUMBERS FROM 0.83 TO 1.36


Descriptive Note : Research memo.


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


Personal Author(s) : JUDD, JOSEPH H ; FALANGA, RALPH A


Full Text : https://apps.dtic.mil/dtic/tr/fulltext/u2/093275.pdf


Report Date : 13 Apr 1956


Pagination or Media Count : 45


Descriptors :   *DELTA WINGS , *FUSELAGES , *JET MIXING FLOW , *DRAG , REDUCTION , PRESSURE


Subject Categories : Aerodynamics


Distribution Statement : APPROVED FOR PUBLIC RELEASE