Hypersonic Flow Theory: Inviscid flows

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ISBN 13 :
Total Pages : 632 pages
Book Rating : 4.:/5 (33 download)

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Book Synopsis Hypersonic Flow Theory: Inviscid flows by : Wallace Dean Hayes

Download or read book Hypersonic Flow Theory: Inviscid flows written by Wallace Dean Hayes and published by . This book was released on 1966 with total page 632 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Hypersonic Strong Interaction Similarity Solutions For Flow Past a Very Slender Axisymmetric Body

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ISBN 13 :
Total Pages : 35 pages
Book Rating : 4.:/5 (632 download)

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Book Synopsis Hypersonic Strong Interaction Similarity Solutions For Flow Past a Very Slender Axisymmetric Body by : Rand Corporation

Download or read book Hypersonic Strong Interaction Similarity Solutions For Flow Past a Very Slender Axisymmetric Body written by Rand Corporation and published by . This book was released on 1966 with total page 35 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Hypersonic Strong Interaction Similarity Solutions for Flow Past and Very Slender Axisymmetric Body

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ISBN 13 :
Total Pages : 46 pages
Book Rating : 4.:/5 (227 download)

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Book Synopsis Hypersonic Strong Interaction Similarity Solutions for Flow Past and Very Slender Axisymmetric Body by : W. B. Bush

Download or read book Hypersonic Strong Interaction Similarity Solutions for Flow Past and Very Slender Axisymmetric Body written by W. B. Bush and published by . This book was released on 1968 with total page 46 pages. Available in PDF, EPUB and Kindle. Book excerpt: The Navier-Stokes hypersonic strong-interaction theory is presented for the flow of a viscous, heat-conducting, compressible fluid past a very slender axisymmetric body, when the ratio of the radius of the body to the radial thickness of the viscous layer(s) (which the body produces and supports), goes to zero. The self-similar leading approximations for the behavior of the flow in these four regions are analyzed, and it is found that an arbitrary body supports '3/4-power' viscous and shock layers. (Author).

Hypersonic Strong Interaction Similarity Solutions for Flow Past a Very Slender Axisymetric Body

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ISBN 13 :
Total Pages : 36 pages
Book Rating : 4.:/5 (78 download)

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Book Synopsis Hypersonic Strong Interaction Similarity Solutions for Flow Past a Very Slender Axisymetric Body by : William B. Bush

Download or read book Hypersonic Strong Interaction Similarity Solutions for Flow Past a Very Slender Axisymetric Body written by William B. Bush and published by . This book was released on 1968 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Viscous Hypersonic Flow Past a Slender Cone

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ISBN 13 :
Total Pages : 20 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis Viscous Hypersonic Flow Past a Slender Cone by : V. S. Nikolaev

Download or read book Viscous Hypersonic Flow Past a Slender Cone written by V. S. Nikolaev and published by . This book was released on 1967 with total page 20 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Hypersonic Weak-interaction Solutions for Flow Past a Very Slender Axisymmetric Body

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ISBN 13 :
Total Pages : 68 pages
Book Rating : 4.:/5 (715 download)

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Book Synopsis Hypersonic Weak-interaction Solutions for Flow Past a Very Slender Axisymmetric Body by : Arthur K. Cross

Download or read book Hypersonic Weak-interaction Solutions for Flow Past a Very Slender Axisymmetric Body written by Arthur K. Cross and published by . This book was released on 1969 with total page 68 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Hypersonic Weak-interaction Solutions for Flow Past a Very Slender Axisymmetric Body

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ISBN 13 :
Total Pages : pages
Book Rating : 4.:/5 (89 download)

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Book Synopsis Hypersonic Weak-interaction Solutions for Flow Past a Very Slender Axisymmetric Body by : Arthur Kent Cross

Download or read book Hypersonic Weak-interaction Solutions for Flow Past a Very Slender Axisymmetric Body written by Arthur Kent Cross and published by . This book was released on 1971 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:

Effect of Body Perturbations on Hypersonic Flow Over Slender Power Law Bodies

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ISBN 13 :
Total Pages : 40 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis Effect of Body Perturbations on Hypersonic Flow Over Slender Power Law Bodies by : Harold Mirels

Download or read book Effect of Body Perturbations on Hypersonic Flow Over Slender Power Law Bodies written by Harold Mirels and published by . This book was released on 1959 with total page 40 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Hypersonic Inviscid Flow

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Publisher : Courier Corporation
ISBN 13 : 0486160483
Total Pages : 628 pages
Book Rating : 4.4/5 (861 download)

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Book Synopsis Hypersonic Inviscid Flow by : Wallace D. Hayes

Download or read book Hypersonic Inviscid Flow written by Wallace D. Hayes and published by Courier Corporation. This book was released on 2012-07-13 with total page 628 pages. Available in PDF, EPUB and Kindle. Book excerpt: Unified, self-contained view of nonequilibrium effects, body geometries, and similitudes available in hypersonic flow and thin shock layer; appropriate for graduate-level courses in hypersonic flow theory. 1966 edition.

Effect of Slight Blunting of Leading Edge of an Immersed Body on the Flow Around it at Hypersonic Speeds

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ISBN 13 :
Total Pages : 24 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis Effect of Slight Blunting of Leading Edge of an Immersed Body on the Flow Around it at Hypersonic Speeds by : Goromir Goromirovich Chernyĭ

Download or read book Effect of Slight Blunting of Leading Edge of an Immersed Body on the Flow Around it at Hypersonic Speeds written by Goromir Goromirovich Chernyĭ and published by . This book was released on 1960 with total page 24 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Axisymmetric Hypersonic Flow with Strong Viscous Interaction

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ISBN 13 :
Total Pages : 50 pages
Book Rating : 4.3/5 (91 download)

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Book Synopsis Axisymmetric Hypersonic Flow with Strong Viscous Interaction by : John Webster Ellinwood

Download or read book Axisymmetric Hypersonic Flow with Strong Viscous Interaction written by John Webster Ellinwood and published by . This book was released on 1967 with total page 50 pages. Available in PDF, EPUB and Kindle. Book excerpt: Stewartson's theory for axisymmetric hypersonic flow of a model gas with strong viscous interaction and strong shock wave is extended to power-law viscosity variation, nonunit Prandtl number, and body shapes other than power laws. For power-law bodies, the generalized theory is obtained in closed form without recourse to numerical integration. In addition, numerical computations are presented for axisymmetric flow over a three-quarter power-law body with strong shock wave and viscous interactions that range from weak to strong. (Author).

Second-order Small-disturbance Solutions for Hypersonic Flow Over Power-law Bodies

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ISBN 13 :
Total Pages : 72 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis Second-order Small-disturbance Solutions for Hypersonic Flow Over Power-law Bodies by : James Courtland Townsend

Download or read book Second-order Small-disturbance Solutions for Hypersonic Flow Over Power-law Bodies written by James Courtland Townsend and published by . This book was released on 1975 with total page 72 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Numerical Solution of the Steady-state Navier-Stokes Equations for Hypersonic Flow about Blunt Axisymmetric Bodies

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ISBN 13 :
Total Pages : 14 pages
Book Rating : 4.:/5 (317 download)

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Book Synopsis Numerical Solution of the Steady-state Navier-Stokes Equations for Hypersonic Flow about Blunt Axisymmetric Bodies by :

Download or read book Numerical Solution of the Steady-state Navier-Stokes Equations for Hypersonic Flow about Blunt Axisymmetric Bodies written by and published by . This book was released on 1974 with total page 14 pages. Available in PDF, EPUB and Kindle. Book excerpt:

On Local Flat-plate Similarity in the Hypersonic Boundary Layer

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ISBN 13 :
Total Pages : 82 pages
Book Rating : 4.E/5 ( download)

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Book Synopsis On Local Flat-plate Similarity in the Hypersonic Boundary Layer by : Franklin Kingston Moore

Download or read book On Local Flat-plate Similarity in the Hypersonic Boundary Layer written by Franklin Kingston Moore and published by . This book was released on 1960 with total page 82 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Similar Solutions for Viscous Hypersonic Flow Over a Slender Three-fourths-power Body of Revolution

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ISBN 13 :
Total Pages : 26 pages
Book Rating : 4.:/5 (317 download)

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Book Synopsis Similar Solutions for Viscous Hypersonic Flow Over a Slender Three-fourths-power Body of Revolution by :

Download or read book Similar Solutions for Viscous Hypersonic Flow Over a Slender Three-fourths-power Body of Revolution written by and published by . This book was released on 1987 with total page 26 pages. Available in PDF, EPUB and Kindle. Book excerpt:

On the Instability of Hypersonic Flow Past a Flat Plate

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ISBN 13 :
Total Pages : 60 pages
Book Rating : 4.:/5 (317 download)

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Book Synopsis On the Instability of Hypersonic Flow Past a Flat Plate by : Institute for Computer Applications in Science and Engineering

Download or read book On the Instability of Hypersonic Flow Past a Flat Plate written by Institute for Computer Applications in Science and Engineering and published by . This book was released on 1990 with total page 60 pages. Available in PDF, EPUB and Kindle. Book excerpt: The instability of hypersonic boundary-layer flows over flat plates is considered. The viscosity of the fluid is taken to be governed by Sutherland's law, which gives a much more accurate representation of the temperature dependence of fluid viscosity at hypersonic speeds than Chapmans's approximate linear law; although at lower speeds the temperature variation of the mean state is less pronounced so that the Chapman law can be used with some confidence. Attention is focussed on the so-called vorticity mode of instability of the viscous hypersonic boundary layer. The instability of the hypersonic boundary layer is non-interactive. The vorticity mode of instability of this flow operates on a significantly different lengthscale than that obtained if a Chapman viscosity law is assumed. The growth rate predicted by a linear viscosity law overestimates the size of the growth rate by O (M-sq). Next, the development of the vorticity mode as the wavenumber decreases is described, and it is shown that acoustic modes emerge when the wavenumber has decreased from it's O(1) initial value to O (M to the -3/2 power). (jhd).

Hypersonic Viscous Interaction on a Slender Body of Revolution with Surface Mass Transfer

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ISBN 13 :
Total Pages : 44 pages
Book Rating : 4.:/5 (227 download)

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Book Synopsis Hypersonic Viscous Interaction on a Slender Body of Revolution with Surface Mass Transfer by : Ting Yi Li

Download or read book Hypersonic Viscous Interaction on a Slender Body of Revolution with Surface Mass Transfer written by Ting Yi Li and published by . This book was released on 1967 with total page 44 pages. Available in PDF, EPUB and Kindle. Book excerpt: An analytical formulation is presented of the problem of hypersonic viscous interaction on a very slender body of revolution with a thick boundary layer and mass transfer. Particular attention is directed to the establishment of the mathematical restrictions necessary to ensure the existence of similar solutions of the laminary boundary-layer equations for this class of problems. Yasuhara's analysis is extended to include surface mass transfer and binary mixture effects. It is shown that when the boundary-layer thickness is of the same order of magnitude as the characteristic body dimension, rigorous similarity is possible only for three-quarter-power-law bodies. This is in agreement with Yasuhara's earlier conclusions. Similar solutions to the boundary-layer growth equations exist when the transverse curvature expression is a function of the similarity variable. The criterion for the existence of similar solutions for the problem of hypersonic viscous interaction is that there must be a definite relationship between body surface shape and surface injection velocity. (Author).