Download or read book Interaction of Weak Shock Waves with Laminar and Turbulent Boundary Layers Analyzed by Momentum integral Method written by Alfred Ritter and published by . This book was released on 1953 with total page 66 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Reflection of a Weak Shock Wave from a Boundary Layer Along a Flat Plate written by Alfred Ritter and published by . This book was released on 1953 with total page 66 pages. Available in PDF, EPUB and Kindle. Book excerpt: This paper is concerned with the phenomena encountered when a plane oblique shock wave is incident upon the boundary layer of a flat plate. In an effort to simplify the problem, the flow field was divided into a viscous layer near the wall and a supersonic potential outer flow. The pressure disturbances due to the incident wave would be propagated upstream and downstream in the subsonic portion of the boundary layer, thus giving rise to perturbations of the boundary layer. By restricting the study to infinitesimal incident compression waves, only small perturbations were encountered and hence the ordinary linearized theory could be applied to the outer flow. In the laminar case, the boundary-layer treatment was based upon a momentum-integral equation previously derived by Howarth. The two flows must be compatible; hence, the deflection of the streamlines near the boundary layer was expressed in terms of the vertical velocity component along the edge of the boundary layer and this relation was used as a boundary condition for the outer flow. The boundary condtion determined the form of solution upstream and downstream of the point of incidence. Determination of the constants of integration was accomplished by a consideration of conditions at infinity and a matching of the two flows at the point of incidence.

Download or read book Investigation of Laminar and Turbulent Boundary Layers Interacting with Externally Generated Shock Waves written by Earl C. Watson and published by . This book was released on 1969 with total page 140 pages. Available in PDF, EPUB and Kindle. Book excerpt: Laminar and turbulent boundary layer interactions with externally generated shock waves.

Download or read book NASA Technical Note written by and published by . This book was released on 1965 with total page 448 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book A Method for Analyzing the Interaction of an Oblique Shock Wave with a Boundary Layer written by William C. Rose and published by . This book was released on 1970 with total page 28 pages. Available in PDF, EPUB and Kindle. Book excerpt: Method for predicting interaction produced by externally generated, oblique shock wave impinging on laminar or turbulent boundary layers.

Download or read book Semiempirical Method for Predicting Effects of Incident reflecting Shocks on the Turbulent Boundary Layer written by Shimer Zane Pinckney and published by . This book was released on 1965 with total page 108 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Technical Note National Advisory Committee for Aeronautics written by United States. National Advisory Committee for Aeronautics and published by . This book was released on 1953 with total page 482 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Monthly Catalog of United States Government Publications written by and published by . This book was released on 1953 with total page 1500 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Subject Index to Unclassified ASTIA Documents written by Defense Documentation Center (U.S.) and published by . This book was released on 1960 with total page 894 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Heat Transfer and Pressure Distribution at a Mach Number of 6 8 on Bodies with Conical Flares and Extensive Flow Separation bJonh V Becker and Peter F Korycinski written by John V. Becker and published by . This book was released on 1962 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Unsteady flow organization of a SWBLI written by Raymond A. Humble and published by Eburon Uitgeverij B.V.. This book was released on 2008 with total page 338 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Boundary Layer Effects in Aerodynamics written by National Physical Laboratory (Great Britain) and published by . This book was released on 1955 with total page 440 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Research Abstracts written by United States. National Advisory Committee for Aeronautics and published by . This book was released on 1951 with total page 568 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Index of NACA Technical Publications written by United States. National Advisory Committee for Aeronautics and published by . This book was released on 1953 with total page 274 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Pakistan Journal of Science written by and published by . This book was released on 1955 with total page 1122 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Scientific and Technical Aerospace Reports written by and published by . This book was released on 1990 with total page 256 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Report written by and published by . This book was released on 1945 with total page 620 pages. Available in PDF, EPUB and Kindle. Book excerpt: