Accession Number : AD0270924
Title : EXPERIMENTAL SEPARATION STUDIES FOR TWO-DIMENSIONAL WEDGES AND CURVED SURFACES AT MACH NUMBERS OF 4.8 TO 6.2
Corporate Author : NATIONAL AERONAUTICS AND SPACE ADMINISTRATION WASHINGTON D C
Personal Author(s) : STERRETT,JAMES R. ; EMERY,JAMES C.
Report Date : FEB 1962
Pagination or Media Count : 1
Abstract : An experimental investigation was made of the separation phenomena on a flat plate at Mach numbers from 4.8 to approximately 6.2. Emphasis was given to determining the maximum pressure ratio obtainable on wedges and curved surfaces without separating the turbulent boundary layer. The effective Reynolds number was changed by using different length plates and by placing roughness strips on the plates. This paper also gives some characteristics of the flow after separation has occurred and gives some insight into body forces associated with separation.
Descriptors : *AERODYNAMIC CHARACTERISTICS, *SHEETS, CURVED PROFILES, FEASIBILITY STUDIES, GASES, MACH NUMBER, PRESSURE, REYNOLDS NUMBER, SEPARATION, SHOCK WAVES, SUPERSONIC FLOW, SURFACE PROPERTIES, TURBULENT BOUNDARY LAYER, WEDGES, WIND TUNNELS
Distribution Statement : APPROVED FOR PUBLIC RELEASE