A Study of Flow Fields about Some Typical Blunt-nosed Slender Bodies

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ISBN 13 :
Total Pages : 122 pages
Book Rating : 4.3/5 (91 download)

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Book Synopsis A Study of Flow Fields about Some Typical Blunt-nosed Slender Bodies by : Roberto Vaglio-Laurin

Download or read book A Study of Flow Fields about Some Typical Blunt-nosed Slender Bodies written by Roberto Vaglio-Laurin and published by . This book was released on 1960 with total page 122 pages. Available in PDF, EPUB and Kindle. Book excerpt:

A Parametric Study of Hypersonic Flow Fields about Blunt-nosed Cylinders at Zero Angle of Attack

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ISBN 13 :
Total Pages : 64 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis A Parametric Study of Hypersonic Flow Fields about Blunt-nosed Cylinders at Zero Angle of Attack by : James E. Terry

Download or read book A Parametric Study of Hypersonic Flow Fields about Blunt-nosed Cylinders at Zero Angle of Attack written by James E. Terry and published by . This book was released on 1964 with total page 64 pages. Available in PDF, EPUB and Kindle. Book excerpt:

NASA Technical Note

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ISBN 13 :
Total Pages : 394 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 1964 with total page 394 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Hypersonic Flow Research

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Publisher : Elsevier
ISBN 13 : 0323142621
Total Pages : 769 pages
Book Rating : 4.3/5 (231 download)

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Book Synopsis Hypersonic Flow Research by : F.R. Riddell

Download or read book Hypersonic Flow Research written by F.R. Riddell and published by Elsevier. This book was released on 2012-12-02 with total page 769 pages. Available in PDF, EPUB and Kindle. Book excerpt: Progress in Astronautics and Rocketry, Volume 7: Hypersonic Flow Research compiles papers presented at a conference on hypersonics held at the Massachusetts Institute of Technology in August 1961. This book discusses the low Reynolds number effects, chemical kinetics effects, inviscid flow calculations, and experimental techniques relating to the problems in acquiring an understanding of hypersonic flow. The structure and composition of hypersonic wakes with attendant complex chemical kinetic effects is only briefly mentioned. This text consists of five parts. Parts A to C comprise of theoretical papers on the problems of calculating flow fields at hypersonic speeds. The experimental techniques that are of immediate practical interest in view of the difficulty of flight testing are discussed in Parts D and E. This publication is beneficial to engineers involved in advanced design problems.

The Downstream Influence of Mass Transfer at the Nose of a Slender Cone

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ISBN 13 :
Total Pages : 56 pages
Book Rating : 4.3/5 (91 download)

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Book Synopsis The Downstream Influence of Mass Transfer at the Nose of a Slender Cone by : Robert J. Cresci

Download or read book The Downstream Influence of Mass Transfer at the Nose of a Slender Cone written by Robert J. Cresci and published by . This book was released on 1962 with total page 56 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Engineering Design Handbook

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ISBN 13 :
Total Pages : 108 pages
Book Rating : 4.:/5 (319 download)

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Book Synopsis Engineering Design Handbook by : United States. Army Materiel Command

Download or read book Engineering Design Handbook written by United States. Army Materiel Command and published by . This book was released on 1965 with total page 108 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Comparison of Experimental and Numerical Results for the Flow of a Perfect Gas about Blunt-nosed Bodies

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ISBN 13 :
Total Pages : 44 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis Comparison of Experimental and Numerical Results for the Flow of a Perfect Gas about Blunt-nosed Bodies by : Mamoru Inouye

Download or read book Comparison of Experimental and Numerical Results for the Flow of a Perfect Gas about Blunt-nosed Bodies written by Mamoru Inouye and published by . This book was released on 1962 with total page 44 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Applied Mechanics Reviews

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ISBN 13 :
Total Pages : 592 pages
Book Rating : 4.:/5 (26 download)

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Book Synopsis Applied Mechanics Reviews by :

Download or read book Applied Mechanics Reviews written by and published by . This book was released on 1974 with total page 592 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Scientific and Technical Aerospace Reports

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ISBN 13 :
Total Pages : 1460 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis Scientific and Technical Aerospace Reports by :

Download or read book Scientific and Technical Aerospace Reports written by and published by . This book was released on 1991 with total page 1460 pages. Available in PDF, EPUB and Kindle. Book excerpt: Lists citations with abstracts for aerospace related reports obtained from world wide sources and announces documents that have recently been entered into the NASA Scientific and Technical Information Database.

NASA Technical Translation

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ISBN 13 :
Total Pages : 804 pages
Book Rating : 4.:/5 (319 download)

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Book Synopsis NASA Technical Translation by :

Download or read book NASA Technical Translation written by and published by . This book was released on 1973 with total page 804 pages. Available in PDF, EPUB and Kindle. Book excerpt:

On the Similar Solutions of Strong Blast-waves and Their Application to Steady Hypersonic Flow

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ISBN 13 :
Total Pages : 184 pages
Book Rating : 4.E/5 ( download)

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Book Synopsis On the Similar Solutions of Strong Blast-waves and Their Application to Steady Hypersonic Flow by : Eric François Brocher

Download or read book On the Similar Solutions of Strong Blast-waves and Their Application to Steady Hypersonic Flow written by Eric François Brocher and published by . This book was released on 1961 with total page 184 pages. Available in PDF, EPUB and Kindle. Book excerpt: The exact 'constant-energy' solution of strong blast waves is expanded in powers of the density ratio across the shock wave; physical quantities are expressed directly as functions of the similitude parameter. The range of validity for t.;e application of this solution to hypersonic flow is then studied as a function of the density ratio. The general similar solution of the strong blast wave is found in the Newtonian approximation. The results are applied to power-law bodies in hypersonic flow using the equivalence principle. The pressure distribution on slender bodies of arbitrary shape is obtained and agrees with the Newton-Busemann pressure formula. Higher-order approximations are derived for the cases in which the shock layer is thin. A simple pressure formula is obtained and some of its applications are shown. (Author).

Progress in Astronautics and Aeronautics

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ISBN 13 :
Total Pages : 1044 pages
Book Rating : 4.3/5 (91 download)

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Book Synopsis Progress in Astronautics and Aeronautics by :

Download or read book Progress in Astronautics and Aeronautics written by and published by . This book was released on 1963 with total page 1044 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Difference Methods for Initial-Boundary-Value Problems and Flow Around Bodies

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Publisher : Springer Science & Business Media
ISBN 13 : 3662067072
Total Pages : 606 pages
Book Rating : 4.6/5 (62 download)

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Book Synopsis Difference Methods for Initial-Boundary-Value Problems and Flow Around Bodies by : You-lan Zhu

Download or read book Difference Methods for Initial-Boundary-Value Problems and Flow Around Bodies written by You-lan Zhu and published by Springer Science & Business Media. This book was released on 2013-06-29 with total page 606 pages. Available in PDF, EPUB and Kindle. Book excerpt: Since the appearance of computers, numerical methods for discontinuous solutions of quasi-linear hyperbolic systems of partial differential equations have been among the most important research subjects in numerical analysis. The authors have developed a new difference method (named the singularity-separating method) for quasi-linear hyperbolic systems of partial differential equations. Its most important feature is that it possesses a high accuracy even for problems with singularities such as schocks, contact discontinuities, rarefaction waves and detonations. Besides the thorough description of the method itself, its mathematical foundation (stability-convergence theory of difference schemes for initial-boundary-value hyperbolic problems) and its application to supersonic flow around bodies are discussed. Further, the method of lines and its application to blunt body problems and conical flow problems are described in detail. This book should soon be an important working basis for both graduate students and researchers in the field of partial differential equations as well as in mathematical physics.

International Aerospace Abstracts

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ISBN 13 :
Total Pages : 1064 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 1969 with total page 1064 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Aerodynamics

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ISBN 13 :
Total Pages : 116 pages
Book Rating : 4.F/5 ( download)

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Book Synopsis Aerodynamics by : United States. Army Materiel Command

Download or read book Aerodynamics written by United States. Army Materiel Command and published by . This book was released on 1965 with total page 116 pages. Available in PDF, EPUB and Kindle. Book excerpt:

U.S. Government Research Reports

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ISBN 13 :
Total Pages : 870 pages
Book Rating : 4.3/5 (243 download)

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Book Synopsis U.S. Government Research Reports by :

Download or read book U.S. Government Research Reports written by and published by . This book was released on 1964 with total page 870 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.