NOL HYPERSONIC TUNNEL NO. 4, RESULTS 7: EXPERIMENTAL INVESTIGATION OF TURBULENT BOUNDARY LAYERS IN HYPERSONIC FLOW.

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ISBN 13 :
Total Pages : 68 pages
Book Rating : 4.:/5 (227 download)

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Book Synopsis NOL HYPERSONIC TUNNEL NO. 4, RESULTS 7: EXPERIMENTAL INVESTIGATION OF TURBULENT BOUNDARY LAYERS IN HYPERSONIC FLOW. by :

Download or read book NOL HYPERSONIC TUNNEL NO. 4, RESULTS 7: EXPERIMENTAL INVESTIGATION OF TURBULENT BOUNDARY LAYERS IN HYPERSONIC FLOW. written by and published by . This book was released on 1955 with total page 68 pages. Available in PDF, EPUB and Kindle. Book excerpt:

NOL Hypersonic Tunnel No. 4 Results VII: Experimental Investiagtion of Turbulent Boundary Layers in Hypersonic Flow

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ISBN 13 :
Total Pages : 40 pages
Book Rating : 4.:/5 (976 download)

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Book Synopsis NOL Hypersonic Tunnel No. 4 Results VII: Experimental Investiagtion of Turbulent Boundary Layers in Hypersonic Flow by : R. Kenneth Lobb

Download or read book NOL Hypersonic Tunnel No. 4 Results VII: Experimental Investiagtion of Turbulent Boundary Layers in Hypersonic Flow written by R. Kenneth Lobb and published by . This book was released on 1955 with total page 40 pages. Available in PDF, EPUB and Kindle. Book excerpt:

NOL Hypersonic Tunnel No. 4

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ISBN 13 :
Total Pages : 84 pages
Book Rating : 4.3/5 (91 download)

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Book Synopsis NOL Hypersonic Tunnel No. 4 by : James E. Danberg

Download or read book NOL Hypersonic Tunnel No. 4 written by James E. Danberg and published by . This book was released on 1964 with total page 84 pages. Available in PDF, EPUB and Kindle. Book excerpt: NOL's Hypersonic Tunnel No. 4 is a continuous blow-down hypersonic tunnel designed for research and development testing of models, instrumentation, and wind tunnel components. It can operate at Mach numbers from 5 to 10 with supply pressures up to 52 atmospheres and supply temperatures up to 1700 R. This report summarizes the pertinent aerodynamic design criteria and operating experience compiled during its first eleven years of operation. Included are descriptions of the major components and their performance along with the flight simulation capability of the facility and a bibliography of previously published reports. (Author).

Analytical, Numerical, and Experimental Results on Turbulent Boundary Layers

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ISBN 13 :
Total Pages : 108 pages
Book Rating : 4.3/5 (91 download)

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Book Synopsis Analytical, Numerical, and Experimental Results on Turbulent Boundary Layers by : David L. Whitfield

Download or read book Analytical, Numerical, and Experimental Results on Turbulent Boundary Layers written by David L. Whitfield and published by . This book was released on 1976 with total page 108 pages. Available in PDF, EPUB and Kindle. Book excerpt: 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).

Technical Report DYN

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ISBN 13 :
Total Pages : 120 pages
Book Rating : 4.X/5 (4 download)

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Book Synopsis Technical Report DYN by :

Download or read book Technical Report DYN written by and published by . This book was released on 1969 with total page 120 pages. Available in PDF, EPUB and Kindle. Book excerpt:

NASA Technical Note

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ISBN 13 :
Total Pages : 1004 pages
Book Rating : 4.:/5 (319 download)

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Book Synopsis NASA Technical Note by :

Download or read book NASA Technical Note written by and published by . This book was released on 1970 with total page 1004 pages. Available in PDF, EPUB and Kindle. Book excerpt:

WADC Technical Report

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ISBN 13 :
Total Pages : 1338 pages
Book Rating : 4.3/5 (91 download)

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Book Synopsis WADC Technical Report by : United States. Wright Air Development Division

Download or read book WADC Technical Report written by United States. Wright Air Development Division and published by . This book was released on 1961 with total page 1338 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Technical Note - National Advisory Committee for Aeronautics

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ISBN 13 :
Total Pages : 690 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis Technical Note - National Advisory Committee for Aeronautics by : United States. National Advisory Committee for Aeronautics

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 1958 with total page 690 pages. Available in PDF, EPUB and Kindle. Book excerpt:

NASA Technical Report

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ISBN 13 :
Total Pages : 50 pages
Book Rating : 4.:/5 (3 download)

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Book Synopsis NASA Technical Report by :

Download or read book NASA Technical Report written by and published by . This book was released on 1961 with total page 50 pages. Available in PDF, EPUB and Kindle. Book excerpt:

OAR Progress

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ISBN 13 :
Total Pages : 670 pages
Book Rating : 4.F/5 ( download)

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Book Synopsis OAR Progress by :

Download or read book OAR Progress written by and published by . This book was released on with total page 670 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Handbook of Supersonic Aerodynamics

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ISBN 13 :
Total Pages : 364 pages
Book Rating : 4.3/5 (91 download)

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Book Synopsis Handbook of Supersonic Aerodynamics by : R. E. Wilson

Download or read book Handbook of Supersonic Aerodynamics written by R. E. Wilson and published by . This book was released on 1966 with total page 364 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Handbook of Supersonic Aerodynamics

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ISBN 13 :
Total Pages : 364 pages
Book Rating : 4.3/5 (91 download)

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Book Synopsis Handbook of Supersonic Aerodynamics by : Johns Hopkins University. Applied Physics Laboratory, Silver Spring, Md

Download or read book Handbook of Supersonic Aerodynamics written by Johns Hopkins University. Applied Physics Laboratory, Silver Spring, Md and published by . This book was released on 1966 with total page 364 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Handbook of Supersonic Aerodynamics

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Publisher :
ISBN 13 :
Total Pages : 364 pages
Book Rating : 4.3/5 (243 download)

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Book Synopsis Handbook of Supersonic Aerodynamics by : Johns Hopkins University. Applied Physics Laboratory

Download or read book Handbook of Supersonic Aerodynamics written by Johns Hopkins University. Applied Physics Laboratory and published by . This book was released on 1966 with total page 364 pages. Available in PDF, EPUB and Kindle. Book excerpt:

OAR

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Publisher :
ISBN 13 :
Total Pages : 168 pages
Book Rating : 4.3/5 (243 download)

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Book Synopsis OAR by :

Download or read book OAR written by and published by . This book was released on 1969 with total page 168 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Power-law Velocity-profile-exponent Variations with Reynolds Number, Wall Cooling, and Mach Number in a Turbulent Boundary Layer

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ISBN 13 :
Total Pages : 66 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis Power-law Velocity-profile-exponent Variations with Reynolds Number, Wall Cooling, and Mach Number in a Turbulent Boundary Layer by : Charles Borden Johnson

Download or read book Power-law Velocity-profile-exponent Variations with Reynolds Number, Wall Cooling, and Mach Number in a Turbulent Boundary Layer written by Charles Borden Johnson and published by . This book was released on 1969 with total page 66 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Preliminary Results of Aerodynamic Heating Studies on the X-15 Airplane

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ISBN 13 :
Total Pages : 22 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis Preliminary Results of Aerodynamic Heating Studies on the X-15 Airplane by : Richard D. Banner

Download or read book Preliminary Results of Aerodynamic Heating Studies on the X-15 Airplane written by Richard D. Banner and published by . This book was released on 1962 with total page 22 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Modern Developments in Gas Dynamics

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Publisher : Springer Science & Business Media
ISBN 13 : 1461586240
Total Pages : 394 pages
Book Rating : 4.4/5 (615 download)

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Book Synopsis Modern Developments in Gas Dynamics by : W. H. Loh

Download or read book Modern Developments in Gas Dynamics written by W. H. Loh and published by Springer Science & Business Media. This book was released on 2012-12-06 with total page 394 pages. Available in PDF, EPUB and Kindle. Book excerpt: During the last decade, the rapid growth of knowledge in the field of fluid mechanics and heat transfer has resulted in many significant ad vances of interest to students, engineers, and scientists. Accordingly, a course entitled "Modern Developments in Fluid Mechanics and Heat Transfer" was given at the University of California to present significant recent theoretical and experimental work. The course consisted of seven parts: I-Introduction; II-Hydraulic Analogy for Gas Dynamics; 111- Turbulence and Unsteady Gas Dynamics; IV-Rarefied and Radiation Gas Dynamics; V-Biological Fluid Mechanics; VI-Hypersonic and Plasma Gas Dynamics; and VII-Heat Transfer in Hypersonic Flows. The material, presented by the undersigned as course instructor and by various guest lecturers, could easily be adapted by other universities for use as a text for a one-semester senior or graduate course on the subject. Due to the extensive notes developed during the University of California course, it was decided to publish the material in three volumes, of which the present is the first. The succeeding volumes will be entitled "Selected Topics in Fluid and Bio-Fluid Mechanics" and "Introduction to Steady and Unsteady Gas Dynamics." Finally, I must express a word of appreciation to my wife Irene and to my children, Wellington Jr. and Victoria, who made it possible for me to write and edit this book in the very quiet atmosphere of our home.