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)
Exploratory Flow Measurements in the Wing-Body Junction of a Possible Mach Four Vehicle
1965
22 pages
Report
Keine Angabe
Englisch
Fluid Mechanics , Aircraft , Missile Technology , 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 , Great Britain
LDV Measurements in the Flow Past a Wing-Body Junction
British Library Conference Proceedings | 1988
|