Author: William Russell Seebaugh
Publisher:
ISBN:
Category :
Languages : en
Pages : 406
Book Description
An Investigation of the Interaction of a Shock Wave and a Turbulent Boundary Layer in Axially Symmetric Internal Flow Including the Effects of Mass Bleed
Author: William Russell Seebaugh
Publisher:
ISBN:
Category :
Languages : en
Pages : 406
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 406
Book Description
NASA Technical Note
An Experimental Investigation of Shock Wave-turbulent Boundary Layer Interactions with and Without Boundary Layer Suction
Author: C. C. Sun
Publisher:
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.
Publisher:
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 Sun
Publisher:
ISBN:
Category : Shock waves
Languages : en
Pages : 916
Book Description
Publisher:
ISBN:
Category : Shock waves
Languages : en
Pages : 916
Book Description
Flowfield Analysis for Successive Oblique Shock Wave-turbulent Boundary Layer Interactions
Author: Chen-Chih Sun
Publisher:
ISBN:
Category : Fluid dynamics
Languages : en
Pages : 116
Book Description
Publisher:
ISBN:
Category : Fluid dynamics
Languages : en
Pages : 116
Book Description
Investigation of Laminar and Turbulent Boundary Layers Interacting with Externally Generated Shock Waves
Author: Earl C. Watson
Publisher:
ISBN:
Category : Laminar boundary layer
Languages : en
Pages : 140
Book Description
Laminar and turbulent boundary layer interactions with externally generated shock waves.
Publisher:
ISBN:
Category : Laminar boundary layer
Languages : en
Pages : 140
Book Description
Laminar and turbulent boundary layer interactions with externally generated shock waves.
Influence of Suction on Shock Wave-turbulent Boundary Layer Interactions for Two-dimensional and Axially Symmetric Flows
Author: William R. Seebaugh
Publisher:
ISBN:
Category : Head waves
Languages : en
Pages : 148
Book Description
Publisher:
ISBN:
Category : Head waves
Languages : en
Pages : 148
Book Description
Papers Presented at the AIAA/ASME/SAE/ASEE 25th Joint Propulsion Conference
American Doctoral Dissertations
Author:
Publisher:
ISBN:
Category : Dissertation abstracts
Languages : en
Pages : 440
Book Description
Publisher:
ISBN:
Category : Dissertation abstracts
Languages : en
Pages : 440
Book Description
The Behavior of a Compressible Turbulent Boundary Layer in a Shock-wave-induced Adverse Pressure Gradient
Author: William C. Rose
Publisher:
ISBN:
Category : Shock waves
Languages : en
Pages : 244
Book Description
Publisher:
ISBN:
Category : Shock waves
Languages : en
Pages : 244
Book Description