Theoretical And Experimental Studies Of Laminar Flow Separation On Flat Plate Wedge Compression Surfaces In The Hypersonic Strong Interaction Regime PDF Download
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Author | : Michael S. Holden |
Publisher | : |
Total Pages | : 178 |
Release | : 1967 |
Genre | : Aerodynamics, Hypersonic |
ISBN | : |
Download Theoretical and Experimental Studies of Laminar Flow Separation on Flat Plate-wedge Compression Surfaces in the Hypersonic Strong Interaction Regime Book in PDF, ePub and Kindle
The report describes a theoretical and experimental investigation of the properties of attached and separated regions of shock wave-laminar boundary layer interactions in the strong interaction regime. A study was made of the flow over a flat plate-wedge compression surface in the high Mach number, low Reynolds number regime where the interaction between the viscous and inviscid regions over the basic flat plate is 'strong' and of fundamental importance to the problem. The theoretical analysis described in the first part of the paper treats the development of the viscous layer and its interaction with the external inviscid stream, using an integral representation for the boundary layer equations. The analysis describes the strong interaction over the flat plate, the transition from a supercritical to a subcritical boundary layer upstream of the separation point, and the subsequent development of the viscous layer through to the end of the interaction. The theory was compared with experimental measurements in both strong and weak interaction regions of separated flow. The complementary experimental study described in the second part of the paper was designed to investigate the shock wave-boundary layer interaction on flat plate-wedge compression surfaces in the strong interaction regime. (Author).
Author | : Michael S. Holden |
Publisher | : |
Total Pages | : 96 |
Release | : 1975 |
Genre | : Aerodynamics, Hypersonic |
ISBN | : |
Download A Study of Flow Separation in Regions of Shock Wave-boundary Layer Interaction in Hypersonic Flow Book in PDF, ePub and Kindle
This report describes a theoretical and experimental investigation of the properties of attached and separated regions of shock wave-laminar boundary layer interacting in the strong interaction regime. The flow is studied over a flat plate-wedge compression surface in the high Mach number, low Reynolds number regime where the interaction between the viscous and inviscid regions over the basic flat plate is strong and of fundamental importance to the problem. The theoretical analysis treats the development of the viscous layer and its interaction with the external inviscid stream, using an integral representation for the boundary layer equations. A complementary experimental study investigated the flow over a flat plate-wedge compression surface for a range of free-stream Reynolds number and Mach number conditions in the strong interaction regime.
Author | : |
Publisher | : |
Total Pages | : 1072 |
Release | : 1976 |
Genre | : Aeronautics |
ISBN | : |
Download Scientific and Technical Aerospace Reports Book in PDF, ePub and Kindle
Author | : |
Publisher | : |
Total Pages | : 0 |
Release | : 1975 |
Genre | : |
ISBN | : |
Download A Study of Flow Separation in Regions of Shock Wave-Boundary Layer Interaction in Hypersonic Flow Book in PDF, ePub and Kindle
This report describes a theoretical and experimental investigation of the properties of attached and separated regions of shock wave-laminar boundary layer interacting in the strong interaction regime. The flow is studied over a flat plate-wedge compression surface in the high Mach number, low Reynolds number regime where the interaction between the viscous and inviscid regions over the basic flat plate is strong and of fundamental importance to the problem. The theoretical analysis treats the development of the viscous layer and its interaction with the external inviscid stream, using an integral representation for the boundary layer equations. A complementary experimental study investigated the flow over a flat plate-wedge compression surface for a range of free-stream Reynolds number and Mach number conditions in the strong interaction regime.
Author | : Defense Documentation Center (U.S.) |
Publisher | : |
Total Pages | : 784 |
Release | : 1967 |
Genre | : Science |
ISBN | : |
Download Technical Abstract Bulletin Book in PDF, ePub and Kindle
Author | : |
Publisher | : Springer Nature |
Total Pages | : 554 |
Release | : 1989 |
Genre | : |
ISBN | : 1468491873 |
Download Hypersonics Book in PDF, ePub and Kindle
Author | : |
Publisher | : |
Total Pages | : 742 |
Release | : 1967 |
Genre | : Mechanics, Applied |
ISBN | : |
Download Applied Mechanics Reviews Book in PDF, ePub and Kindle
Author | : Bernard G. Gautier |
Publisher | : |
Total Pages | : 100 |
Release | : 1971 |
Genre | : Boundary layer |
ISBN | : |
Download A Theoretical Study of Wall Cooling Effects Upon Shock Wave-laminar Boundary Layer Interaction by the Method of Lees-reeves-klineberg Book in PDF, ePub and Kindle
Author | : Raymond Brun |
Publisher | : Springer Science & Business Media |
Total Pages | : 497 |
Release | : 2012-12-06 |
Genre | : Science |
ISBN | : 3642788297 |
Download Shock Waves @ Marseille I Book in PDF, ePub and Kindle
Recently, there have been significant advances in the fields of high-enthalpy hypersonic flows, high-temperature gas physics, and chemistry shock propagation in various media, industrial and medical applications of shock waves, and shock-tube technology. This series contains all the papers and lectures of the 19th International Symposium on Shock Waves held in Marseille in 1993. They are published in four topical volumes, each containing papers on related topics, and preceded by an overview written by a leading international expert. The volumes may be purchased independently.
Author | : |
Publisher | : |
Total Pages | : 1062 |
Release | : 1967 |
Genre | : Government publications |
ISBN | : |
Download Government-wide Index to Federal Research & Development Reports Book in PDF, ePub and Kindle