Accession Number : AD0654684

Title :   EXPERIMENTAL RESULTS FOR MASSIVE BLOWING STUDIES.

Descriptive Note : Rept. for Jun 65-Jun 66,

Corporate Author : AEROSPACE CORP EL SEGUNDO CALIF LAB OPERATIONS

Personal Author(s) : Hartunian,R. A. ; Spencer,D. J.

Report Date : APR 1967

Pagination or Media Count : 38

Abstract : Previous work on the problem of massive blowing is described. A technique for visualizing the streamline separating the blown gas from that of the oncoming stream is developed, in which a chemiluminescent reaction along the separation streamline appears as a yellow glow and is easily photographed. Data for a variety of aerodynamic shapes over a wide range of flow conditions were obtained. A major result is that the separation streamline is essentially straight for a wedge- or cone-shaped model. Pressure distributions measured on the surface of wedge and cone models indicate that the pressure decays from high values near the leading edge of blowing to low values near the trailing edge. (Author)

Descriptors :   (*AERODYNAMICS, FLOW VISUALIZATION), AERODYNAMIC CONFIGURATIONS, FLOW SEPARATION, CONICAL BODIES, CYLINDRICAL BODIES, LEADING EDGES, WEDGES, INJECTION

Subject Categories : Aerodynamics
      Fluid Mechanics

Distribution Statement : APPROVED FOR PUBLIC RELEASE