Overview of X-38 Hypersonic Thermodynamic Wind Tunnel Data and Comparison with Numerical Results

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ISBN 13 :
Total Pages : pages
Book Rating : 4.:/5 (11 download)

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Book Synopsis Overview of X-38 Hypersonic Thermodynamic Wind Tunnel Data and Comparison with Numerical Results by : Charles H. Campbell

Download or read book Overview of X-38 Hypersonic Thermodynamic Wind Tunnel Data and Comparison with Numerical Results written by Charles H. Campbell and published by . This book was released on 1997 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:

Overview of X-38 Hypersonic Wind Tunnel Data and Comparison with Numerical Results

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ISBN 13 :
Total Pages : pages
Book Rating : 4.:/5 (11 download)

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Book Synopsis Overview of X-38 Hypersonic Wind Tunnel Data and Comparison with Numerical Results by : Charles H. Campbell

Download or read book Overview of X-38 Hypersonic Wind Tunnel Data and Comparison with Numerical Results written by Charles H. Campbell and published by . This book was released on 1997 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:

Numerical Study of Rarefied Hypersonic Flow Interacting with a Continuum Jet

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ISBN 13 :
Total Pages : 224 pages
Book Rating : 4.:/5 (317 download)

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Book Synopsis Numerical Study of Rarefied Hypersonic Flow Interacting with a Continuum Jet by : Christopher E. Glass

Download or read book Numerical Study of Rarefied Hypersonic Flow Interacting with a Continuum Jet written by Christopher E. Glass and published by . This book was released on 2000 with total page 224 pages. Available in PDF, EPUB and Kindle. Book excerpt: An uncoupled CFD-DSMC technique is developed and applied to provide solutions for continuum jets interacting with rarefield external flows. The technique is based on a correlation of the appropriate Bird breakdown parameter for a transitional-rarefield condition that defines a surface within which the continuum solution is unaffected by the external flow-jet interaction. The method is applied to two problems to assess and demonstrate its validity: one of a jet interaction in the transitional-rarefied flow regime and the other in the moderately rarefield regime. Results show that the appropriate Bird breakdown surface for uncoupling the continuum and non-continuum solutions is a function of a non-dimensional parameter relating the momentum flux and collisionality between the two interacting flows.

32nd Thermophysics Conference

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ISBN 13 :
Total Pages : 734 pages
Book Rating : 4.0/5 ( download)

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Book Synopsis 32nd Thermophysics Conference by :

Download or read book 32nd Thermophysics Conference written by and published by . This book was released on 1997 with total page 734 pages. Available in PDF, EPUB and Kindle. Book excerpt:

A Variable Atmosphere Hypersonic Wind Tunnel for Similitude Studies

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ISBN 13 :
Total Pages : 64 pages
Book Rating : 4.E/5 ( download)

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Book Synopsis A Variable Atmosphere Hypersonic Wind Tunnel for Similitude Studies by : G. M. Gregorek

Download or read book A Variable Atmosphere Hypersonic Wind Tunnel for Similitude Studies written by G. M. Gregorek and published by . This book was released on 1966 with total page 64 pages. Available in PDF, EPUB and Kindle. Book excerpt:

36th Aerospace Sciences Meeting & Exhibit

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ISBN 13 :
Total Pages : 644 pages
Book Rating : 4.0/5 ( download)

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Book Synopsis 36th Aerospace Sciences Meeting & Exhibit by :

Download or read book 36th Aerospace Sciences Meeting & Exhibit written by and published by . This book was released on 1998 with total page 644 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Results of Aerothermodynamic and Boundary-Layer Transition Testing of 0.0362-Scale X-38 (Rev. 3.1) Vehicle in NASA Langley 20-Inch Mach 6 Tunnel

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ISBN 13 :
Total Pages : 102 pages
Book Rating : 4.:/5 (317 download)

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Book Synopsis Results of Aerothermodynamic and Boundary-Layer Transition Testing of 0.0362-Scale X-38 (Rev. 3.1) Vehicle in NASA Langley 20-Inch Mach 6 Tunnel by :

Download or read book Results of Aerothermodynamic and Boundary-Layer Transition Testing of 0.0362-Scale X-38 (Rev. 3.1) Vehicle in NASA Langley 20-Inch Mach 6 Tunnel written by and published by . This book was released on 1997 with total page 102 pages. Available in PDF, EPUB and Kindle. Book excerpt:

X-33 Computational Aeroheating/Aerodynamic Predictions and Comparisons With Experimental Data

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ISBN 13 :
Total Pages : 90 pages
Book Rating : 4.:/5 (317 download)

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Book Synopsis X-33 Computational Aeroheating/Aerodynamic Predictions and Comparisons With Experimental Data by : Brian Ray Hollis

Download or read book X-33 Computational Aeroheating/Aerodynamic Predictions and Comparisons With Experimental Data written by Brian Ray Hollis and published by . This book was released on 2003 with total page 90 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Selected Aerothermodynamic Design Problems of Hypersonic Flight Vehicles

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Publisher : Springer Science & Business Media
ISBN 13 : 354089974X
Total Pages : 512 pages
Book Rating : 4.5/5 (48 download)

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Book Synopsis Selected Aerothermodynamic Design Problems of Hypersonic Flight Vehicles by : Ernst Heinrich Hirschel

Download or read book Selected Aerothermodynamic Design Problems of Hypersonic Flight Vehicles written by Ernst Heinrich Hirschel and published by Springer Science & Business Media. This book was released on 2009-11-26 with total page 512 pages. Available in PDF, EPUB and Kindle. Book excerpt: In this book selected aerothermodynamic design problems in hypersonic vehicles are treated. Where applicable, it emphasizes the fact that outer surfaces of hypersonic vehicles primarily are radiation-cooled, an interdisciplinary topic with many implications.

NASA Langley Scientific and Technical Information Output: 1997

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ISBN 13 :
Total Pages : 162 pages
Book Rating : 4.:/5 (317 download)

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Book Synopsis NASA Langley Scientific and Technical Information Output: 1997 by :

Download or read book NASA Langley Scientific and Technical Information Output: 1997 written by and published by . This book was released on 1998 with total page 162 pages. Available in PDF, EPUB and Kindle. Book excerpt:

The High Temperature Aspects of Hypersonic Flow

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Publisher : Elsevier
ISBN 13 : 1483223310
Total Pages : 801 pages
Book Rating : 4.4/5 (832 download)

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Book Synopsis The High Temperature Aspects of Hypersonic Flow by : Wilbur C. Nelson

Download or read book The High Temperature Aspects of Hypersonic Flow written by Wilbur C. Nelson and published by Elsevier. This book was released on 2014-12-02 with total page 801 pages. Available in PDF, EPUB and Kindle. Book excerpt: The High Temperature Aspects of Hypersonic Flow is a record of the proceedings of the AGARD-NATO Specialists' Meeting, held at the Technical Centre for Experimental Aerodynamics, Rhode-Saint-Genese, Belgium in April 1962. The book contains the papers presented during the meeting that tackled a broad range of topics in the aspects of hypersonic flow. The subjects covered during the meeting include pressure measurements, interference effects, the use of wind tunnels in aircraft development testing, high temperature gas characteristics, boundary layer research, stability and control and the use of rocket vehicles in flight research. Aerospace engineers and aeronautical engineers will find the book invaluable.

Scientific and Technical Aerospace Reports

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ISBN 13 :
Total Pages : 372 pages
Book Rating : 4.:/5 (319 download)

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International Aerospace Abstracts

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ISBN 13 :
Total Pages : 974 pages
Book Rating : 4.F/5 ( download)

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Book Synopsis International Aerospace Abstracts by :

Download or read book International Aerospace Abstracts written by and published by . This book was released on 1999 with total page 974 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Hypersonic and High Temperature Gas Dynamics

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Publisher : AIAA
ISBN 13 : 9781563474590
Total Pages : 710 pages
Book Rating : 4.4/5 (745 download)

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Book Synopsis Hypersonic and High Temperature Gas Dynamics by : John David Anderson

Download or read book Hypersonic and High Temperature Gas Dynamics written by John David Anderson and published by AIAA. This book was released on 1989 with total page 710 pages. Available in PDF, EPUB and Kindle. Book excerpt: This book is a self-contained text for those students and readers interested in learning hypersonic flow and high-temperature gas dynamics. It assumes no prior familiarity with either subject on the part of the reader. If you have never studied hypersonic and/or high-temperature gas dynamics before, and if you have never worked extensively in the area, then this book is for you. On the other hand, if you have worked and/or are working in these areas, and you want a cohesive presentation of the fundamentals, a development of important theory and techniques, a discussion of the salient results with emphasis on the physical aspects, and a presentation of modern thinking in these areas, then this book is also for you. In other words, this book is designed for two roles: 1) as an effective classroom text that can be used with ease by the instructor, and understood with ease by the student; and 2) as a viable, professional working tool for engineers, scientists, and managers who have any contact in their jobs with hypersonic and/or high-temperature flow.

A Comparison of Hypersonic Wind Tunnel Data Obtained by Static and Free Oscillation Techniques

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ISBN 13 :
Total Pages : 7 pages
Book Rating : 4.:/5 (976 download)

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Book Synopsis A Comparison of Hypersonic Wind Tunnel Data Obtained by Static and Free Oscillation Techniques by : K. F. Stetson

Download or read book A Comparison of Hypersonic Wind Tunnel Data Obtained by Static and Free Oscillation Techniques written by K. F. Stetson and published by . This book was released on 1977 with total page 7 pages. Available in PDF, EPUB and Kindle. Book excerpt:

34th AIAA Thermophysics Conference

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ISBN 13 :
Total Pages : 460 pages
Book Rating : 4.0/5 ( download)

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Book Synopsis 34th AIAA Thermophysics Conference by :

Download or read book 34th AIAA Thermophysics Conference written by and published by . This book was released on 2000 with total page 460 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Comparison of Wind Tunnel and Flight Data for a Hypersonic Instrumentation Rocket

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ISBN 13 :
Total Pages : pages
Book Rating : 4.:/5 (958 download)

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Download or read book Comparison of Wind Tunnel and Flight Data for a Hypersonic Instrumentation Rocket written by and published by . This book was released on 1964 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt: