Numerical Analysis of Flow Properties about Blunt Bodies Moving at Supersonic Speeds in an Equilibrium Gas

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ISBN 13 :
Total Pages : 96 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis Numerical Analysis of Flow Properties about Blunt Bodies Moving at Supersonic Speeds in an Equilibrium Gas by : Harvard Lomax

Download or read book Numerical Analysis of Flow Properties about Blunt Bodies Moving at Supersonic Speeds in an Equilibrium Gas written by Harvard Lomax and published by . This book was released on 1964 with total page 96 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Numerical Analysis of Flow Properties about Blunt Bodies Moving at SUpersonic Speeds in an Equilibriumm Gas

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ISBN 13 :
Total Pages : 79 pages
Book Rating : 4.:/5 (633 download)

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Book Synopsis Numerical Analysis of Flow Properties about Blunt Bodies Moving at SUpersonic Speeds in an Equilibriumm Gas by : Harvard Lomax

Download or read book Numerical Analysis of Flow Properties about Blunt Bodies Moving at SUpersonic Speeds in an Equilibriumm Gas written by Harvard Lomax and published by . This book was released on 1964 with total page 79 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Calculation of Axisymmetric Supersonic Flow Past Blunt Bodies with Sonic Corners

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

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Book Synopsis Calculation of Axisymmetric Supersonic Flow Past Blunt Bodies with Sonic Corners by : Jerry Curtis South

Download or read book Calculation of Axisymmetric Supersonic Flow Past Blunt Bodies with Sonic Corners written by Jerry Curtis South and published by . This book was released on 1968 with total page 66 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Experimental Study of the Shock Wave Due to a Blunt Leading Edge in the Hypersonic Merged-flow Regime

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ISBN 13 :
Total Pages : 28 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis Experimental Study of the Shock Wave Due to a Blunt Leading Edge in the Hypersonic Merged-flow Regime by : Roger M. Winebarger

Download or read book Experimental Study of the Shock Wave Due to a Blunt Leading Edge in the Hypersonic Merged-flow Regime written by Roger M. Winebarger and published by . This book was released on 1970 with total page 28 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Deduction of Reentry Plasma Properties about Manned Orbital Spacecraft from Radio Signal Attenuation Data

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

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Book Synopsis Deduction of Reentry Plasma Properties about Manned Orbital Spacecraft from Radio Signal Attenuation Data by : Paul W. Huber

Download or read book Deduction of Reentry Plasma Properties about Manned Orbital Spacecraft from Radio Signal Attenuation Data written by Paul W. Huber and published by . This book was released on 1967 with total page 44 pages. Available in PDF, EPUB and Kindle. Book excerpt:

NASA Technical Paper

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ISBN 13 :
Total Pages : 84 pages
Book Rating : 4.F/5 ( download)

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Book Synopsis NASA Technical Paper by :

Download or read book NASA Technical Paper written by and published by . This book was released on 1979 with total page 84 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Numerical Results for the Diffraction of a Normal Shock Wave by a Sphere and for the Subsequent Transient Flow

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

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Book Synopsis Numerical Results for the Diffraction of a Normal Shock Wave by a Sphere and for the Subsequent Transient Flow by : Richard W. Barnwell

Download or read book Numerical Results for the Diffraction of a Normal Shock Wave by a Sphere and for the Subsequent Transient Flow written by Richard W. Barnwell and published by . This book was released on 1967 with total page 44 pages. Available in PDF, EPUB and Kindle. Book excerpt: The finite-difference method which Peter D. Lax developed for treating unsteady inviscid flow fields is used to study the transient flow in the shock layer of a sphere that has been struck by a normal shock wave. Transient flow of this sort is encountered when a shock tube is used as a supersonic wind tunnel. Time histories of the shock detachment distance and the stagnation-point pressure and tangential velocity gradient are presented for ranges of the incident-shock Mach number and the perfect-gas specific-heat ratio. These results show that the stagnation-point pressure approaches the steady value much more rapidly than the shock detachment distance. In general, the stagnation-point pressure but more rapidly than the shock detachment distance. As the specific-heat ratio is decreased and the incident-shock Mach number is increased, the variation of the velocity gradient with respect to the shock detachment distance becomes more nearly linear.

Compressible Turbulent Boundary Layers

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ISBN 13 :
Total Pages : 580 pages
Book Rating : 4.X/5 (4 download)

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Book Synopsis Compressible Turbulent Boundary Layers by :

Download or read book Compressible Turbulent Boundary Layers written by and published by . This book was released on 1969 with total page 580 pages. Available in PDF, EPUB and Kindle. Book excerpt:

NASA Technical Note

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ISBN 13 :
Total Pages : 418 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 1975 with total page 418 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Inviscid Radiating Shock Layers about Spheres Traveling at Hyperbolic Speeds in Air

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ISBN 13 :
Total Pages : 88 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis Inviscid Radiating Shock Layers about Spheres Traveling at Hyperbolic Speeds in Air by : Richard W. Barnwell

Download or read book Inviscid Radiating Shock Layers about Spheres Traveling at Hyperbolic Speeds in Air written by Richard W. Barnwell and published by . This book was released on 1969 with total page 88 pages. Available in PDF, EPUB and Kindle. Book excerpt: Time-dependent finite-difference techniques are used to obtain numerical solutions for the problem of the inviscid flow of radiating equilibrium air past sphere traveling at hyperbolic speeds. The effects of absorption are included, and results are presented for both gray and nongray absorption coefficient models for spheres with different radii. It is shown that the nondimensional heat-flux distributions for the gray and nongray models are similar and that these distributions are weak functions of the radius of the sphere and the altitude and strong functions of the flight velocity.

Effect of Unit Reynolds Number, Nose Bluntness, Angle of Attack, and Roughness on Transition on a 5° Half-angle Cone at Mach 8

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ISBN 13 :
Total Pages : 82 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis Effect of Unit Reynolds Number, Nose Bluntness, Angle of Attack, and Roughness on Transition on a 5° Half-angle Cone at Mach 8 by : P. Calvin Stainback

Download or read book Effect of Unit Reynolds Number, Nose Bluntness, Angle of Attack, and Roughness on Transition on a 5° Half-angle Cone at Mach 8 written by P. Calvin Stainback and published by . This book was released on 1969 with total page 82 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Impact of Aerospace Technology on Studies of the Earth's Atmosphere

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Publisher : Elsevier
ISBN 13 : 1483147819
Total Pages : 261 pages
Book Rating : 4.4/5 (831 download)

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Book Synopsis Impact of Aerospace Technology on Studies of the Earth's Atmosphere by : A.K. Oppenheim

Download or read book Impact of Aerospace Technology on Studies of the Earth's Atmosphere written by A.K. Oppenheim and published by Elsevier. This book was released on 2013-10-22 with total page 261 pages. Available in PDF, EPUB and Kindle. Book excerpt: Impact of Aerospace Technology on Studies of the Earth's Atmosphere is a 13-chapter book that describes the studies that use space-based instruments to explore many qualities of the atmosphere. This text presents the studies about the Earth's magnetosphere, ionosphere, stratosphere, mesosphere, climate, and pollution. The International Magnetospheric Study is also covered. The use of fluorescent ion jets, lasers, space vehicles, and equipments on board Concorde 001 in this field of interest is explained as well. This book will be very useful as a base from which all nations can think out their own programs of equipment, measurement, and use in the study of Earth's atmosphere.

A Bibliography for the Numerical Solution of Partial Differential Equations

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ISBN 13 :
Total Pages : 126 pages
Book Rating : 4.F/5 ( download)

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Book Synopsis A Bibliography for the Numerical Solution of Partial Differential Equations by : John H. Giese

Download or read book A Bibliography for the Numerical Solution of Partial Differential Equations written by John H. Giese and published by . This book was released on 1969 with total page 126 pages. Available in PDF, EPUB and Kindle. Book excerpt: A list of 2561 references to the numerical solution of partial differential equations has been compiled. References to reviews in several abstracting journals have been given, and a crude index has been prepared. (Author).

On Hypersonic Blunt Body Flow Fields Obtained with a Time-dependent Technique

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ISBN 13 :
Total Pages : 78 pages
Book Rating : 4.3/5 (91 download)

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Book Synopsis On Hypersonic Blunt Body Flow Fields Obtained with a Time-dependent Technique by : John David Anderson (Jr.)

Download or read book On Hypersonic Blunt Body Flow Fields Obtained with a Time-dependent Technique written by John David Anderson (Jr.) and published by . This book was released on 1968 with total page 78 pages. Available in PDF, EPUB and Kindle. Book excerpt: New results are presented for inviscid, supersonic and hypersonic blunt-body flow fields obtained with a numerical time-dependent method patterned after that of Moretti and Abbett. In addition, important comments are made with regard to the physical and numerical nature of the method. Specifically, numerical results are presented for two-dimensional and axisymmetric parabolic and cubic blunt bodies as well as blunted wedges and cones; these results are presented for zero degrees angle of attack and for a calorically perfect gas with gamma = 1.4. The numerical results are compared with other existing theoretical and experimental data. Also, the effects of initial conditions and boundary conditions are systematically examined with regard to the convergence of the time-dependent numerical solutions, and the point is made that the initial conditions can not be completely arbitrary. Finally, in order to learn more about the performance of the time-dependent method, a numerical experiment is conducted to examine the unsteady propagation and region of influence of a slight pressure disturbance introduced at a point on the surface of a blunt body.

NASA Technical Report

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ISBN 13 :
Total Pages : 630 pages
Book Rating : 4.:/5 (319 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 1971 with total page 630 pages. Available in PDF, EPUB and Kindle. Book excerpt:

NASA Technical Memorandum

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ISBN 13 :
Total Pages : 264 pages
Book Rating : 4.:/5 (319 download)

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Book Synopsis NASA Technical Memorandum by :

Download or read book NASA Technical Memorandum written by and published by . This book was released on 1981 with total page 264 pages. Available in PDF, EPUB and Kindle. Book excerpt:

A Method of Integral Relations Solution for Radiating, Nonadiabatic, Inviscid Flow Over a Blunt Body

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ISBN 13 :
Total Pages : 68 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis A Method of Integral Relations Solution for Radiating, Nonadiabatic, Inviscid Flow Over a Blunt Body by : John Timothy Suttles

Download or read book A Method of Integral Relations Solution for Radiating, Nonadiabatic, Inviscid Flow Over a Blunt Body written by John Timothy Suttles and published by . This book was released on 1969 with total page 68 pages. Available in PDF, EPUB and Kindle. Book excerpt: