Heat Transfer at the Forward Stagnation Point of Blunt Bodies

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ISBN 13 :
Total Pages : 17 pages
Book Rating : 4.:/5 (248 download)

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Book Synopsis Heat Transfer at the Forward Stagnation Point of Blunt Bodies by : Eli Reshotko

Download or read book Heat Transfer at the Forward Stagnation Point of Blunt Bodies written by Eli Reshotko and published by . This book was released on 1955 with total page 17 pages. Available in PDF, EPUB and Kindle. Book excerpt: Relations are presented for the calculation of heat transfer at the forward stagnation point of both two-dimensional and axially symmetric blunt bodies. The relations for the heat transfer, which were obtained from exact solutions to the equations of the laminar boundary layer, are presented in terms of the local velocity gradient at the stagnation point. These exact solutions include the effects of variation of fluid properties, Prandtl number, and transpiration cooling. Examples illustrating the calculation procedure are also included.

Experimental Stagnation-point Velocity Gradients and Heat-transfer Coefficients for a Family of Blunt Bodies at Mach 8 and Angles of Attack

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ISBN 13 :
Total Pages : 32 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis Experimental Stagnation-point Velocity Gradients and Heat-transfer Coefficients for a Family of Blunt Bodies at Mach 8 and Angles of Attack by : James C. Ellison

Download or read book Experimental Stagnation-point Velocity Gradients and Heat-transfer Coefficients for a Family of Blunt Bodies at Mach 8 and Angles of Attack written by James C. Ellison and published by . This book was released on 1969 with total page 32 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Heat-transfer Characteristics of Blunt Two-and Three-dimensional Bodies at Supersonic Speeds

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ISBN 13 :
Total Pages : 22 pages
Book Rating : 4.3/5 (91 download)

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Book Synopsis Heat-transfer Characteristics of Blunt Two-and Three-dimensional Bodies at Supersonic Speeds by : Glen Goodwin

Download or read book Heat-transfer Characteristics of Blunt Two-and Three-dimensional Bodies at Supersonic Speeds written by Glen Goodwin and published by . This book was released on 1956 with total page 22 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Stagnation-point Shielding by Melting and Vaporization

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ISBN 13 :
Total Pages : 36 pages
Book Rating : 4.:/5 (317 download)

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Book Synopsis Stagnation-point Shielding by Melting and Vaporization by : Leonard Roberts

Download or read book Stagnation-point Shielding by Melting and Vaporization written by Leonard Roberts and published by . This book was released on 1959 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt: An approximate theoretical analysis is made of the shielding mechanism whereby the rate of heat transfer to the forward stagnation point of blunt bodies is reduced by melting and vaporization. General qualitative results are given and a numerical example, the melting and vaporization of ice, is presented and discussed in detail.

An Approximate Analysis of Unsteady Vaporization Near the Stagnation Point of Blunt Bodies

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ISBN 13 :
Total Pages : 38 pages
Book Rating : 4.:/5 (317 download)

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Book Synopsis An Approximate Analysis of Unsteady Vaporization Near the Stagnation Point of Blunt Bodies by : Leonard Roberts

Download or read book An Approximate Analysis of Unsteady Vaporization Near the Stagnation Point of Blunt Bodies written by Leonard Roberts and published by . This book was released on 1959 with total page 38 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Stagnation Point Heat Transfer Predictions for Blunt Bodies in Hypervelocity Flow

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ISBN 13 :
Total Pages : 33 pages
Book Rating : 4.:/5 (227 download)

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Book Synopsis Stagnation Point Heat Transfer Predictions for Blunt Bodies in Hypervelocity Flow by : Peter A. Ross

Download or read book Stagnation Point Heat Transfer Predictions for Blunt Bodies in Hypervelocity Flow written by Peter A. Ross and published by . This book was released on 1964 with total page 33 pages. Available in PDF, EPUB and Kindle. Book excerpt: Stagnation point heat transfer predictions from boundary layer program by E.A. Brown and A. Dusto are presented in comparison with other predictions and shock tube data. Several charts have been prepared in terms of simulation parameters, whereby, the heating rates based on these results can be quickly determined at the stagnation point of a blunt body in shock tubes, hypervelocity tunnels and gun ranges. (Author).

Duplication of Reynolds Number and Stagnation Point Heat Transfer Rates for Blunt Bodies at Hypersonic Speeds

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

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Book Synopsis Duplication of Reynolds Number and Stagnation Point Heat Transfer Rates for Blunt Bodies at Hypersonic Speeds by : J. D. Regan

Download or read book Duplication of Reynolds Number and Stagnation Point Heat Transfer Rates for Blunt Bodies at Hypersonic Speeds written by J. D. Regan and published by . This book was released on 1973 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:

Heat Transfer Analysis Without and with Forward Facing Spike Attached to a Blunt Body at High Speed Flow

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ISBN 13 :
Total Pages : pages
Book Rating : 4.:/5 (115 download)

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Book Synopsis Heat Transfer Analysis Without and with Forward Facing Spike Attached to a Blunt Body at High Speed Flow by : Rakhab Chandra Mehta

Download or read book Heat Transfer Analysis Without and with Forward Facing Spike Attached to a Blunt Body at High Speed Flow written by Rakhab Chandra Mehta and published by . This book was released on 2018 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt: The present chapter deals with heat transfer analysis around unspiked and spiked bodies at high speeds. A spike attached to a blunt-nosed body drastically alters its flowfield and influences the aerodynamic heating in a high speed flow. The effect of spike length, shape and spike-nose configuration is numerically studied at zero angle of incidence. The numerical analysis describes overall flowfield features over without and with forward facing spike attached to a blunt body at high speed flow. The shock stand-off distance, sonic line, stagnation point velocity gradient and stagnation point heat flux are analyzed and compared with different aerodisk configurations. It is found that the hemispherical aerodisk experiences high wall heat flux as compared to the flat-faced aerodisk. Numerical and experimental studies reveal that the wall heat flux levels are decreased in the presence of the spikes and aerospike as compared to without attached spiked to the blunt-nose basic configuration.

Technical Note - National Advisory Committee for Aeronautics

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ISBN 13 :
Total Pages : 1160 pages
Book Rating : 4.E/5 ( download)

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Book Synopsis Technical Note - National Advisory Committee for Aeronautics by : United States. National Advisory Committee for Aeronautics

Download or read book Technical Note - National Advisory Committee for Aeronautics written by United States. National Advisory Committee for Aeronautics and published by . This book was released on 1958 with total page 1160 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Stagnation-point Shielding by Melting and Vaporization

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ISBN 13 :
Total Pages : 24 pages
Book Rating : 4.:/5 (346 download)

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Book Synopsis Stagnation-point Shielding by Melting and Vaporization by : Leonard Roberts

Download or read book Stagnation-point Shielding by Melting and Vaporization written by Leonard Roberts and published by . This book was released on 1959 with total page 24 pages. Available in PDF, EPUB and Kindle. Book excerpt: An approximate theoretical analysis is made of the shielding mechanism whereby the rate of heat transfer to the forward stagnation point of blunt bodies is reduced by melting and vaporization. General qualitative results are given and a numerical example, the melting and vaporization of ice, is presented and discussed in detail.

Mass Transfer Cooling Near the Stagnation Point

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ISBN 13 :
Total Pages : 24 pages
Book Rating : 4.:/5 (317 download)

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Book Synopsis Mass Transfer Cooling Near the Stagnation Point by : Leonard Roberts

Download or read book Mass Transfer Cooling Near the Stagnation Point written by Leonard Roberts and published by . This book was released on 1959 with total page 24 pages. Available in PDF, EPUB and Kindle. Book excerpt: A simplified analysis is made of mass transfer cooling--that is, injection of a foreign gas--near the stagnation point for two-dimensional and axisymmetric bodies. The reduction in heat transfer is given in terms of the properties of the coolant gas and it is shown that the heat transfer may be reduced considerably by the introduction of a gas having appropriate thermal and diffusive properties. The mechanism by which heat transfer is reduced is discussed.

Report

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

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Book Synopsis Report by : United States. National Advisory Committee for Aeronautics

Download or read book Report written by United States. National Advisory Committee for Aeronautics and published by . This book was released on 1957 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt:

NASA Technical Note

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ISBN 13 :
Total Pages : 402 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 1972 with total page 402 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Hypersonic Flow Theory

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Publisher : Elsevier
ISBN 13 : 032314876X
Total Pages : 481 pages
Book Rating : 4.3/5 (231 download)

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Book Synopsis Hypersonic Flow Theory by : Wallace Hayes

Download or read book Hypersonic Flow Theory written by Wallace Hayes and published by Elsevier. This book was released on 2012-12-02 with total page 481 pages. Available in PDF, EPUB and Kindle. Book excerpt: Hypersonic Flow Theory presents the fundamentals of fluid mechanics, focusing on the hypersonic flow theory and approaches in theoretical aerodynamics. This book discusses the assumptions underlying hypersonic flow theory, unified supersonic-hypersonic similitude, two-dimensional and axisymmetric bodies, and circular cylinder. The constant-streamtube-area approximation, streamtube-continuity methods, and tangent-wedge and tangent-cone are also deliberated. This text likewise covers the similar laminar boundary layer solutions, bluntness induced interactions on slender bodies, and free molecule transfer theory. The dynamics of hypersonic flight or hypersonic wing theory, magnetohydrodynamic theory, or any developments involving treatment of the Boltzmann equation are not included. This publication is intended for hypersonic aerodynamicists, students, and researchers conducting work on the hypersonic flow phenomena.

Scientific and Technical Aerospace Reports

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ISBN 13 :
Total Pages : 1040 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 1973 with total page 1040 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.

Study of High-density Hypervelocity Flows and Similitudes

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ISBN 13 :
Total Pages : 320 pages
Book Rating : 4.E/5 ( download)

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Book Synopsis Study of High-density Hypervelocity Flows and Similitudes by : Cornell Aeronautical Laboratory

Download or read book Study of High-density Hypervelocity Flows and Similitudes written by Cornell Aeronautical Laboratory and published by . This book was released on 1967 with total page 320 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Subject Index to Unclassified ASTIA Documents

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ISBN 13 :
Total Pages : 922 pages
Book Rating : 4.3/5 (91 download)

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Book Synopsis Subject Index to Unclassified ASTIA Documents by : Defense Documentation Center (U.S.)

Download or read book Subject Index to Unclassified ASTIA Documents written by Defense Documentation Center (U.S.) and published by . This book was released on 1960 with total page 922 pages. Available in PDF, EPUB and Kindle. Book excerpt: