Stagnation Point Heat Transfer in a Relaxing Gas

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

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Book Synopsis Stagnation Point Heat Transfer in a Relaxing Gas by : Robert Elliott Wilson

Download or read book Stagnation Point Heat Transfer in a Relaxing Gas written by Robert Elliott Wilson and published by . This book was released on 1963 with total page 108 pages. Available in PDF, EPUB and Kindle. Book excerpt: Stagnation point heat transfer in a gas undergoing relaxation of its internal energy is examined by solution of the equations of motion using the two temperature approach of Wang Chang and Uhlenbeck. The results are presented in parametric form and show that relaxation effects produce an adiabatic wall temperature above the free stream stagnation temperature, which is related to the thermal conductivity of the ''inert" mode, the dimensionless relaxation length, the ratio of the translational mode temperature to the temperature of the relaxing mode at the edge of the boundary layer, and the magnitude of the internal energy undergoing relaxation. An experiment is described whereby the thermal conductivity of the "inert" mode, which is unknown, may be determined from adiabatic wall temperature measurements.

Stagnation Point Heat Transfer in a Relaxing Gas

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ISBN 13 :
Total Pages : 0 pages
Book Rating : 4.:/5 (184 download)

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Book Synopsis Stagnation Point Heat Transfer in a Relaxing Gas by : Robert Elliot Wilson

Download or read book Stagnation Point Heat Transfer in a Relaxing Gas written by Robert Elliot Wilson and published by . This book was released on 1963 with total page 0 pages. Available in PDF, EPUB and Kindle. Book excerpt: Stagnation point heat transfer in a gas undergoing relaxation of its internal energy is examined by solution of the equations of motion using the two temperature approach of Wang Chang and Uhlenbeck. The results are presented in parametric form and show that relaxation effects produce an adiabatic wall temperature above the free stream stagnation temperature, which is related to the thermal conducitivity of the inert mode, the dimensionless relaxation length, the ratio of the translational mode temperature to the temperature of the relaxing mode at the edge of the boundary layer, and the magnitude of the internal energy undergoing relaxation. An experiment is described whereby the thermal conductivity of the inert mode, which is unknown, may be determined from adiabatic wall temperature measurements. (Author).

Stagnation Point Heat Transfer in a Partially Ionized Gas

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ISBN 13 :
Total Pages : 124 pages
Book Rating : 4.F/5 ( download)

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Book Synopsis Stagnation Point Heat Transfer in a Partially Ionized Gas by : Richard Walter Rutowski

Download or read book Stagnation Point Heat Transfer in a Partially Ionized Gas written by Richard Walter Rutowski and published by . This book was released on 1959 with total page 124 pages. Available in PDF, EPUB and Kindle. Book excerpt:

A Theoretical Study of Stagnation-point Ablation

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

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Book Synopsis A Theoretical Study of Stagnation-point Ablation by : Leonard Roberts

Download or read book A Theoretical Study of Stagnation-point Ablation written by Leonard Roberts and published by . This book was released on 1959 with total page 20 pages. Available in PDF, EPUB and Kindle. Book excerpt: A simplified analysis is made of ablation cooling near the stagnation point of a two-dimensional or axisymmetric body which occurs as the body vaporizes directly from the solid state. The automatic shielding mechanism is discussed and the important thermal properties required by a good ablation material are given. The results of the analysis are given in terms of dimensionless parameters.

Empirical Stagnation-point Heat-transfer Relation in Several Gas Mixtures at High Enthalpy Levels

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ISBN 13 :
Total Pages : 26 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis Empirical Stagnation-point Heat-transfer Relation in Several Gas Mixtures at High Enthalpy Levels by : Ernest V. Zoby

Download or read book Empirical Stagnation-point Heat-transfer Relation in Several Gas Mixtures at High Enthalpy Levels written by Ernest V. Zoby and published by . This book was released on 1968 with total page 26 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Scientific and Technical Aerospace Reports

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ISBN 13 :
Total Pages : 742 pages
Book Rating : 4.3/5 (91 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 1976 with total page 742 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 Scientific and Technical Reports

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ISBN 13 :
Total Pages : 966 pages
Book Rating : 4.F/5 ( download)

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Book Synopsis NASA Scientific and Technical Reports by : United States. National Aeronautics and Space Administration Scientific and Technical Information Division

Download or read book NASA Scientific and Technical Reports written by United States. National Aeronautics and Space Administration Scientific and Technical Information Division and published by . This book was released on 1970 with total page 966 pages. Available in PDF, EPUB and Kindle. Book excerpt:

A Thin-shock-layer Solution for Nonequilibrium, Inviscid Hypersonic Flows in Earth, Martian, and Venusian Atmospheres

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ISBN 13 :
Total Pages : 164 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis A Thin-shock-layer Solution for Nonequilibrium, Inviscid Hypersonic Flows in Earth, Martian, and Venusian Atmospheres by : William L. Gose

Download or read book A Thin-shock-layer Solution for Nonequilibrium, Inviscid Hypersonic Flows in Earth, Martian, and Venusian Atmospheres written by William L. Gose and published by . This book was released on 1971 with total page 164 pages. Available in PDF, EPUB and Kindle. Book excerpt: An approximate inverse solution is presented for the nonequilibrium flow in the inviscid shock layer about a vehicle in hypersonic flight. The method is based upon a thin-shock-layer approximation and has the advantage of being applicable to both subsonic and supersonic regions of the shock layer. The relative simplicity of the method makes it ideally suited for programming on a digital computer with a significant reduction in storage capacity and computing time required by other more exact methods. Comparison of nonequilibrium solutions for an air mixture obtained by the present method is made with solutions obtained by two other methods. Additional cases are presented for entry of spherical nose cones into representative Venusian and Martian atmospheres. A digital computer program written in FORTRAN language is presented that permits an arbitrary gas mixture to be employed in the solution. The effects of vibration, dissociation, recombination, electronic excitation, and ionization are included in the program.

NASA Technical Note

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ISBN 13 :
Total Pages : 358 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 1962 with total page 358 pages. Available in PDF, EPUB and Kindle. Book excerpt:

U.S. Government Research Reports

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ISBN 13 :
Total Pages : 1416 pages
Book Rating : 4.3/5 (91 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 1416 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Stagnation Point Flow and Heat Transfer Under Free-stream Turbulence

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ISBN 13 :
Total Pages : 234 pages
Book Rating : 4.3/5 (91 download)

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Book Synopsis Stagnation Point Flow and Heat Transfer Under Free-stream Turbulence by : Zhongmin Xiong

Download or read book Stagnation Point Flow and Heat Transfer Under Free-stream Turbulence written by Zhongmin Xiong and published by . This book was released on 2004 with total page 234 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Shock Waves

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Publisher : Springer Science & Business Media
ISBN 13 : 3540851682
Total Pages : 810 pages
Book Rating : 4.5/5 (48 download)

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Book Synopsis Shock Waves by : Klaus Hannemann

Download or read book Shock Waves written by Klaus Hannemann and published by Springer Science & Business Media. This book was released on 2009-04-01 with total page 810 pages. Available in PDF, EPUB and Kindle. Book excerpt: The 26th International Symposium on Shock Waves in Göttingen, Germany was jointly organised by the German Aerospace Centre DLR and the French-German Research Institute of Saint Louis ISL. The year 2007 marked the 50th anniversary of the Symposium, which first took place in 1957 in Boston and has since become an internationally acclaimed series of meetings for the wider Shock Wave Community. The ISSW26 focused on the following areas: Shock Propagation and Reflection, Detonation and Combustion, Hypersonic Flow, Shock Boundary Layer Interaction, Numerical Methods, Medical, Biological and Industrial Applications, Richtmyer Meshkov Instability, Blast Waves, Chemically Reacting Flows, Diagnostics, Facilities, Flow Visualisation, Ignition, Impact and Compaction, Multiphase Flow, Nozzles Flows, Plasmas and Propulsion. The two Volumes contain the papers presented at the symposium and serve as a reference for the participants of the ISSW 26 and individuals interested in these fields.

Survey of Heat Transfer to Near-critical Fluids

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ISBN 13 :
Total Pages : 124 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis Survey of Heat Transfer to Near-critical Fluids by : Robert C. Hendricks

Download or read book Survey of Heat Transfer to Near-critical Fluids written by Robert C. Hendricks and published by . This book was released on 1970 with total page 124 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Design and Calibration of an Arc-heated, Hypersonic, Low-density Wind Tunnel

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ISBN 13 :
Total Pages : 36 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis Design and Calibration of an Arc-heated, Hypersonic, Low-density Wind Tunnel by : Ruth N. Weitmann

Download or read book Design and Calibration of an Arc-heated, Hypersonic, Low-density Wind Tunnel written by Ruth N. Weitmann and published by . This book was released on 1962 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Effects of Unsteady Free Stream Velocity and Free Stream Turbulence on Stagnation Point Heat Transfer

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ISBN 13 :
Total Pages : 42 pages
Book Rating : 4.F/5 ( download)

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Book Synopsis Effects of Unsteady Free Stream Velocity and Free Stream Turbulence on Stagnation Point Heat Transfer by : Rama S. R. Gorla

Download or read book Effects of Unsteady Free Stream Velocity and Free Stream Turbulence on Stagnation Point Heat Transfer written by Rama S. R. Gorla and published by . This book was released on 1984 with total page 42 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Technical Abstract Bulletin

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ISBN 13 :
Total Pages : 828 pages
Book Rating : 4.E/5 ( download)

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Book Synopsis Technical Abstract Bulletin by :

Download or read book Technical Abstract Bulletin written by and published by . This book was released on with total page 828 pages. Available in PDF, EPUB and Kindle. Book excerpt:

A Review of Some Recent Developments in Hypersonic Flow

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ISBN 13 :
Total Pages : 90 pages
Book Rating : 4.3/5 (91 download)

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Book Synopsis A Review of Some Recent Developments in Hypersonic Flow by : Antonio Ferri

Download or read book A Review of Some Recent Developments in Hypersonic Flow written by Antonio Ferri and published by . This book was released on 1958 with total page 90 pages. Available in PDF, EPUB and Kindle. Book excerpt: