Accession Number : AD0093071


Title :   SUPERSONIC-AREA-RULE DESIGN AND ROCKET-PROPELLED FLIGHT INVESTIGATION OF A ZERO-LIFT STRAIGHT-WING-BODY-NACELLE CONFIGURATION BETWEEN MACH NUMBERS 0.8 AND 1.53


Descriptive Note : Research memo.


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


Personal Author(s) : HOFFMAN, SHERWOOD


Full Text : https://apps.dtic.mil/dtic/tr/fulltext/u2/093071.pdf


Report Date : 26 Apr 1956


Pagination or Media Count : 33


Descriptors :   *WING BODY CONFIGURATIONS , *SUPERSONIC FLOW , *NACELLES , WINGS , FUSELAGES , REDUCTION , DRAG


Subject Categories : Aerodynamics


Distribution Statement : APPROVED FOR PUBLIC RELEASE