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Experimental And Numerical Investigation Of Boundary Layer Development And Transition On The Walls Of A Mach 5 Nozzle Book in PDF, ePub and Kindle version is available to download in english. Read online anytime anywhere directly from your device. Click on the download button below to get a free pdf file of Experimental And Numerical Investigation Of Boundary Layer Development And Transition On The Walls Of A Mach 5 Nozzle book. This book definitely worth reading, it is an incredibly well-written.
Author : Anonim
Publisher : Unknown
Page : 1932 pages
File Size : 48,9 Mb
Release : 1976
Category : Government publications
ISBN : STANFORD:36105006328988
Author : United States. Superintendent of Documents
Publisher : Unknown
Page : 1320 pages
File Size : 53,7 Mb
Release : 1966
Category : Government publications
ISBN : WISC:89035089036
Author : United States. Superintendent of Documents
Publisher : Unknown
Page : 1348 pages
File Size : 44,6 Mb
Release : 1970
Category : United States
ISBN : STANFORD:36105019598304
Author : Anonim
Publisher : Unknown
Page : 616 pages
File Size : 49,6 Mb
Release : 1975
Category : Electronic
ISBN : MINN:319510008465407
Author : William D. Harvey,Aubrey M. Cary,Julius E. Harris
Publisher : Unknown
Page : 92 pages
File Size : 42,7 Mb
Release : 1975
Category : Aerodynamics, Hypersonic
ISBN : UIUC:30112106917096
Author : Anonim
Publisher : Unknown
Page : 836 pages
File Size : 48,7 Mb
Release : 1994
Category : Aeronautics
ISBN : UIUC:30112067190055
Author : Anonim
Publisher : Unknown
Page : 568 pages
File Size : 40,5 Mb
Release : 1973
Category : Mechanics, Applied
ISBN : UCAL:C2682441
Author : William D. Harvey,William W. Hunter
Publisher : Unknown
Page : 76 pages
File Size : 41,9 Mb
Release : 1975
Category : Aerodynamics, Hypersonic
ISBN : UIUC:30112106917062
Author : Anonim
Publisher : Unknown
Page : 46 pages
File Size : 53,5 Mb
Release : 1981
Category : Electronic
ISBN : NASA:31769000551104
Author : Anonim
Publisher : Unknown
Page : 644 pages
File Size : 55,6 Mb
Release : 1976
Category : Aeronautics
ISBN : UOM:39015010883455
Author : Anonim
Publisher : Unknown
Page : 492 pages
File Size : 41,8 Mb
Release : 1994
Category : Aeronautics
ISBN : MINN:31951P00691495X
Author : Anthony W. Fiore
Publisher : Unknown
Page : 962 pages
File Size : 48,5 Mb
Release : 1978
Category : Turbulent boundary layer
ISBN : UOM:39015095313683
In 1975 the U.S. Air Force and the Federal Republic of Germany signed a Data Exchange Agreement numbered AF-75-G-7440 entitled 'Viscous and Interacting Flow Fields.' The purpose was to exchange data in the area of boundary layer research. It includes both experimental and theoretical boundary layer research at speeds from subsonic to hypersonic Mach numbers in the presence of laminar, transitional, and turbulent boundary layers. The main effort in recent years has been on turbulent boundary layers, both attached and separated in the presence of such parameters as pressure gradients, wall temperature, surface roughness, etc. In the United States the research was conducted in various Department of Defense, NASA, aircraft corporations, and various university laboratories. In the Federal Republic of Germany it was carried out within the various DFVLR, industrial, and university research centers.
Author : David L. Whitfield
Publisher : Unknown
Page : 108 pages
File Size : 40,6 Mb
Release : 1976
Category : Laminar boundary layer
ISBN : UOM:39015104952422
This report describes the results of analytical, numerical, and experimental investigations of incompressible and compressible boundary layers. The subjects considered are (1) Laminar and/or turbulent numerical boundary-layer calculations in which the Reynolds stress is related to the turbulent kinetic energy; (2) an analytical investigation of turbulence near a wall which is not founded on classical mixing-length theory; (3) analytical solutions for relating velocity and temperature throughout turbulent boundary layers for nonunity Prandtl numbers; (4) a description of the data reduction of pitot pressure measurements utilizing these analytical results, and (5) the application of the numerical and analytical results to the analysis of turbulent boundary-layer measurements made in the Propulsion Wind Tunnel Facility (PWT).
Author : United States. Congress. Senate. Select Committee on Small Business
Publisher : Unknown
Page : 1440 pages
File Size : 46,9 Mb
Release : 1975
Category : Legislative hearings
ISBN : UCAL:B3608359
Author : United States. Congress. Senate. Select Committee on Small Business
Publisher : Unknown
Page : 572 pages
File Size : 49,9 Mb
Release : 1976
Category : Government publications
ISBN : PURD:32754078073727