Author: Publisher:
ISBN:
Category :
Languages : en
Pages : 452
Book Description
NASA Technical Note
An Experimental Investigation of Shock Wave-turbulent Boundary Layer Interactions with and Without Boundary Layer Suction
Author: C. C. SunPublisher:
ISBN:
Category : Shock waves
Languages : en
Pages : 916
Book Description
Tabulated data from a series of experimental studies of the interaction of a shock wave with a turbulent boundary layer in axisymmetric flow configurations is presented. The studies were conducted at the walls of circular wind tunnels and on the cylindrical centerbody of an annular flow channel. Detailed pitot pressure profiles and wall static pressure profiles upstream of, within and downstream of the interaction region are given. Results are presented for flows at nominal freestream Mach Numbers of 2, 3 and 4. For studies at the tunnel sidewalls, the shock waves were produced by conical shock generators mounted on the centerline of the wind tunnel at zero angle of attack. The annular ring generator was used to produce the shock wave at the centerbody of the annular flow channel. The effects of boundary layer bleed were examined in the investigation. Both bleed rate and bleed location were studied. Most of the bleed studies were conducted with bleed holes drilled normal to the wall surface but the effects of slot suction were also examined. A summary of the principal results and conclusions is given.
An experimental investigation of shock wave-turbulent boundary layer interactions with and without boundary layer suction
Author: Chen-Chih SunPublisher:
ISBN:
Category : Shock waves
Languages : en
Pages : 916
Book Description
Papers Presented at the AIAA/ASME/SAE/ASEE 25th Joint Propulsion Conference
Author: Flowfield Analysis for Successive Oblique Shock Wave-turbulent Boundary Layer Interactions
Author: Chen-Chih SunPublisher:
ISBN:
Category : Fluid dynamics
Languages : en
Pages : 116
Book Description
A Collection of Technical Papers
Author: The Behavior of a Compressible Turbulent Boundary Layer in a Shock-wave-induced Adverse Pressure Gradient
Author: William C. RosePublisher:
ISBN:
Category : Shock waves
Languages : en
Pages : 244
Book Description
American Doctoral Dissertations
Author: Publisher:
ISBN:
Category : Dissertation abstracts
Languages : en
Pages : 440
Book Description
NASA Contractor Report
Author: United States. National Aeronautics and Space AdministrationPublisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 936
Book Description
Author: