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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

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 PDF 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

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 PDF Author: William Russell Seebaugh
Publisher:
ISBN:
Category :
Languages : en
Pages : 406

Book Description


NASA Technical Note

NASA Technical Note PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 452

Book Description


An Experimental Investigation of Shock Wave-turbulent Boundary Layer Interactions with and Without Boundary Layer Suction

An Experimental Investigation of Shock Wave-turbulent Boundary Layer Interactions with and Without Boundary Layer Suction PDF 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.

An experimental investigation of shock wave-turbulent boundary layer interactions with and without boundary layer suction

An experimental investigation of shock wave-turbulent boundary layer interactions with and without boundary layer suction PDF Author: Chen-Chih Sun
Publisher:
ISBN:
Category : Shock waves
Languages : en
Pages : 916

Book Description


Flowfield Analysis for Successive Oblique Shock Wave-turbulent Boundary Layer Interactions

Flowfield Analysis for Successive Oblique Shock Wave-turbulent Boundary Layer Interactions PDF Author: Chen-Chih Sun
Publisher:
ISBN:
Category : Fluid dynamics
Languages : en
Pages : 116

Book Description


Investigation of Laminar and Turbulent Boundary Layers Interacting with Externally Generated Shock Waves

Investigation of Laminar and Turbulent Boundary Layers Interacting with Externally Generated Shock Waves PDF 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.

Influence of Suction on Shock Wave-turbulent Boundary Layer Interactions for Two-dimensional and Axially Symmetric Flows

Influence of Suction on Shock Wave-turbulent Boundary Layer Interactions for Two-dimensional and Axially Symmetric Flows PDF Author: William R. Seebaugh
Publisher:
ISBN:
Category : Head waves
Languages : en
Pages : 148

Book Description


Papers Presented at the AIAA/ASME/SAE/ASEE 25th Joint Propulsion Conference

Papers Presented at the AIAA/ASME/SAE/ASEE 25th Joint Propulsion Conference PDF Author:
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 442

Book Description


American Doctoral Dissertations

American Doctoral Dissertations PDF Author:
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

The Behavior of a Compressible Turbulent Boundary Layer in a Shock-wave-induced Adverse Pressure Gradient PDF Author: William C. Rose
Publisher:
ISBN:
Category : Shock waves
Languages : en
Pages : 244

Book Description