Accession Number : AD0478914


Title :   EXPLORATORY FLOW MEASUREMENTS IN THE WING-BODY JUNCTION OF A POSSIBLE MACH FOUR VEHICLE.


Descriptive Note : Technical rept.,


Corporate Author : ROYAL AIRCRAFT ESTABLISHMENT FARNBOROUGH (UNITED KINGDOM)


Personal Author(s) : Roe, P L


Report Date : Nov 1965


Pagination or Media Count : 23


Abstract : Measurements of flow direction, total pressure, and Mach number were made near a possible engine inlet location in the wing-body junction of a projected high-speed vehicle layout. An undesirable feature of the flow is the presence of a vortex in the corner of the junction. (Author)


Descriptors :   *WING BODY CONFIGURATIONS , SUPERSONIC CHARACTERISTICS , FLOW FIELDS , PRESSURE , AIRSPEED , JET ENGINE INLETS , VORTICES , DELTA WINGS , SUPERSONIC FLOW , DEFLECTION , WIND TUNNEL MODELS , MODEL TESTS , PERFORMANCE(ENGINEERING) , EXPERIMENTAL DATA , ANGLE OF ATTACK , YAW , UNITED KINGDOM


Subject Categories : Aircraft
      Guided Missiles
      Fluid Mechanics


Distribution Statement : APPROVED FOR PUBLIC RELEASE