Experimental Investigation Of The Interaction Of A Plane Oblique Incident Reflecting Shock Wave With A Turbulent Boundary Layer On A Cooled Surface Volume 1 Test Description And Data Summary PDF Download
Are you looking for read ebook online? Search for your book and save it on your Kindle device, PC, phones or tablets. Download Experimental Investigation Of The Interaction Of A Plane Oblique Incident Reflecting Shock Wave With A Turbulent Boundary Layer On A Cooled Surface Volume 1 Test Description And Data Summary PDF full book. Access full book title Experimental Investigation Of The Interaction Of A Plane Oblique Incident Reflecting Shock Wave With A Turbulent Boundary Layer On A Cooled Surface Volume 1 Test Description And Data Summary.
Author | : |
Publisher | : |
Total Pages | : 88 |
Release | : 1969 |
Genre | : |
ISBN | : |
Download Experimental Investigation of the Interaction of a Plane, Oblique, Incident-reflecting Shock Wave with a Turbulent Boundary Layer on a Cooled Surface. Volume 1 - Test Description and Data Summary Book in PDF, ePub and Kindle
Author | : |
Publisher | : |
Total Pages | : 316 |
Release | : 1969 |
Genre | : |
ISBN | : |
Download Experimental Investigation of the Interaction of a Plane, Oblique, Incident-reflecting Shock Wave with a Turbulent Boundary Layer on a Cooled Surface. Volume 3 - Tabulated Data Book in PDF, ePub and Kindle
Author | : |
Publisher | : |
Total Pages | : 192 |
Release | : 1969 |
Genre | : |
ISBN | : |
Download Experimental Investigation of the Interaction of a Plane, Oblique, Incident-reflecting Shock Wave with a Turbulent Boundary Layer on a Cooled Surface. Volume 2 - Basic Plotted Data Book in PDF, ePub and Kindle
Author | : |
Publisher | : |
Total Pages | : 892 |
Release | : 1994 |
Genre | : Aeronautics |
ISBN | : |
Download Scientific and Technical Aerospace Reports Book in PDF, ePub and Kindle
Author | : Amado Arthur Trujillo |
Publisher | : |
Total Pages | : 254 |
Release | : 1962 |
Genre | : |
ISBN | : |
Download Experimental Investigation of the Interaction of an Oblique Shock Wave with a Turbulent Boundary Layer Book in PDF, ePub and Kindle
Author | : Chen-Chih Sun |
Publisher | : |
Total Pages | : 916 |
Release | : 1977 |
Genre | : Shock waves |
ISBN | : |
Download An experimental investigation of shock wave-turbulent boundary layer interactions with and without boundary layer suction Book in PDF, ePub and Kindle
Author | : Earl C. Watson |
Publisher | : |
Total Pages | : 140 |
Release | : 1969 |
Genre | : Laminar boundary layer |
ISBN | : |
Download Investigation of Laminar and Turbulent Boundary Layers Interacting with Externally Generated Shock Waves Book in PDF, ePub and Kindle
Laminar and turbulent boundary layer interactions with externally generated shock waves.
Author | : S. Z. Pinckney |
Publisher | : |
Total Pages | : 220 |
Release | : 1966 |
Genre | : Aerodynamics, Hypersonic |
ISBN | : |
Download Data on Effects of Incident-reflecting Shocks on the Turbulent Boundary Layer Book in PDF, ePub and Kindle
Author | : David William Kuntz |
Publisher | : |
Total Pages | : 544 |
Release | : 1985 |
Genre | : |
ISBN | : |
Download An Experimental Investigation of the Shock Wave-turbulent Boundary Layer Interaction Book in PDF, ePub and Kindle
Author | : C. C. Sun |
Publisher | : |
Total Pages | : 916 |
Release | : 1977 |
Genre | : Shock waves |
ISBN | : |
Download An Experimental Investigation of Shock Wave-turbulent Boundary Layer Interactions with and Without Boundary Layer Suction Book in PDF, ePub and Kindle
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.