A New Method for Studying Leading Edge Heat Transfer in Supersonic Flow ByH.Y.Wong

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Book Synopsis A New Method for Studying Leading Edge Heat Transfer in Supersonic Flow ByH.Y.Wong by : H.Y. Wong

Download or read book A New Method for Studying Leading Edge Heat Transfer in Supersonic Flow ByH.Y.Wong written by H.Y. Wong and published by . This book was released on 1979 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:

A New Method for Studying Leading Edge Heat Transfer in Supersonic Flow

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Total Pages : 45 pages
Book Rating : 4.:/5 (11 download)

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Book Synopsis A New Method for Studying Leading Edge Heat Transfer in Supersonic Flow by : H. Y. Wong

Download or read book A New Method for Studying Leading Edge Heat Transfer in Supersonic Flow written by H. Y. Wong and published by . This book was released on 1979 with total page 45 pages. Available in PDF, EPUB and Kindle. Book excerpt:

A Review of High-speed, Convective, Heat-transfer Computation Methods

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

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Book Synopsis A Review of High-speed, Convective, Heat-transfer Computation Methods by : Michael E. Tauber

Download or read book A Review of High-speed, Convective, Heat-transfer Computation Methods written by Michael E. Tauber and published by . This book was released on 1989 with total page 44 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Evaluation of Two Theoretical Methods for the Prediction of Heat Transfer to the Leading Edge of a Swept Wing in Supersonic Flow

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Total Pages : 98 pages
Book Rating : 4.:/5 (24 download)

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Book Synopsis Evaluation of Two Theoretical Methods for the Prediction of Heat Transfer to the Leading Edge of a Swept Wing in Supersonic Flow by : Clinton Dinty Winant (Jr)

Download or read book Evaluation of Two Theoretical Methods for the Prediction of Heat Transfer to the Leading Edge of a Swept Wing in Supersonic Flow written by Clinton Dinty Winant (Jr) and published by . This book was released on 1967 with total page 98 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Scientific and Technical Aerospace Reports

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ISBN 13 :
Total Pages : 440 pages
Book Rating : 4.:/5 (3 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 1995 with total page 440 pages. Available in PDF, EPUB and Kindle. Book excerpt:

A Correlation of Leading Edge Transition and Heat Transfer on Swept Cylinders in Supersonic Flow

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Total Pages : 9 pages
Book Rating : 4.:/5 (11 download)

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Book Synopsis A Correlation of Leading Edge Transition and Heat Transfer on Swept Cylinders in Supersonic Flow by : D. R. Topham

Download or read book A Correlation of Leading Edge Transition and Heat Transfer on Swept Cylinders in Supersonic Flow written by D. R. Topham and published by . This book was released on 1964 with total page 9 pages. Available in PDF, EPUB and Kindle. Book excerpt:

OAR Cumulative Index of Research Results

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ISBN 13 :
Total Pages : 1264 pages
Book Rating : 4.3/5 (243 download)

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Book Synopsis OAR Cumulative Index of Research Results by :

Download or read book OAR Cumulative Index of Research Results written by and published by . This book was released on 1967 with total page 1264 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Results of Supersonic Heat-Transfer Studies on Blunt Swept Leading Edges

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Total Pages : 58 pages
Book Rating : 4.:/5 (227 download)

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Book Synopsis Results of Supersonic Heat-Transfer Studies on Blunt Swept Leading Edges by : Albert F Gollnick (Jr)

Download or read book Results of Supersonic Heat-Transfer Studies on Blunt Swept Leading Edges written by Albert F Gollnick (Jr) and published by . This book was released on 1970 with total page 58 pages. Available in PDF, EPUB and Kindle. Book excerpt: Stagnation-line heat-transfer distributions were obtained on blunt swept leading edges at Mach 3.66 and a Reynolds number per foot of 210,000. Pressure distributions were obtained for comparable test conditions. The results illustrate the effects of various flow nonuniformities on leading-edge heat transfer and pressure, including those arising from finite span and nonuniform leading-edge sweep; free-stream nonuniformity induced by the bow shock of typical blunt body; boundary-layer interaction near the leading-edge root; and impingement of a trailing-tip vortex. None of these effects can be predicted analytically as yet, and all may lead to significant deviation from the levels based on infinite-cylinder theory. The importance of the individual results are discussed, and, where possible, appropriate design criteria are presented. (Author).

Hypersonic Engine Leading Edge Experiments in a High Heat Flux, Supersonic Flow Environment

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Total Pages : 18 pages
Book Rating : 4.:/5 (317 download)

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Book Synopsis Hypersonic Engine Leading Edge Experiments in a High Heat Flux, Supersonic Flow Environment by :

Download or read book Hypersonic Engine Leading Edge Experiments in a High Heat Flux, Supersonic Flow Environment written by and published by . This book was released on 1994 with total page 18 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Aeronautical Engineering

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ISBN 13 :
Total Pages : 538 pages
Book Rating : 4.3/5 (91 download)

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Download or read book Aeronautical Engineering written by and published by . This book was released on 1991 with total page 538 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:

Examination of the Existing Data on the Heat Transfer of Turbulent Boundary Layers at Supersonic Speeds from the Point of View of Reynolds Analogy

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Total Pages : 654 pages
Book Rating : 4.F/5 ( download)

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Book Synopsis Examination of the Existing Data on the Heat Transfer of Turbulent Boundary Layers at Supersonic Speeds from the Point of View of Reynolds Analogy by : Alvin Seiff

Download or read book Examination of the Existing Data on the Heat Transfer of Turbulent Boundary Layers at Supersonic Speeds from the Point of View of Reynolds Analogy written by Alvin Seiff and published by . This book was released on 1954 with total page 654 pages. Available in PDF, EPUB and Kindle. Book excerpt: Heat-transfer data from four wind-tunnel experiments and two free-flight experiments with turbulent boundary layers have been examined to see whether or not they are well represented by the Reynolds analogy or a modification thereof. The heat-transfer results are put into the form of dimensionless Stanton numbers based on fluid properties at the outer edge of the boundary layer and are compared with skin-friction coefficients for the same Mach numbers and wall to free-stream temperature ratios as obtained from an interpolation of the existing skin-friction data. The effective Reynolds number is taken to be the length Reynolds number measured from the effective turbulent origin, a position which differs importantly from the leading edge of the test surface in some cases.

NASA SP.

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ISBN 13 :
Total Pages : 548 pages
Book Rating : 4.:/5 (319 download)

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Book Synopsis NASA SP. by :

Download or read book NASA SP. written by and published by . This book was released on 1992 with total page 548 pages. Available in PDF, EPUB and Kindle. Book excerpt:

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 Selected Listing of NASA Scientific and Technical Reports

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ISBN 13 :
Total Pages : 962 pages
Book Rating : 4.E/5 ( download)

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

Download or read book A Selected Listing of 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 962 pages. Available in PDF, EPUB and Kindle. Book excerpt:

NASA Scientific and Technical Reports and Publications for 1969 - A Selected Listing

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ISBN 13 :
Total Pages : 956 pages
Book Rating : 4.:/5 (317 download)

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Book Synopsis NASA Scientific and Technical Reports and Publications for 1969 - A Selected Listing by : United States. National Aeronautics and Space Administration. Scientific and Technical Information Division

Download or read book NASA Scientific and Technical Reports and Publications for 1969 - A Selected Listing 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 956 pages. Available in PDF, EPUB and Kindle. Book excerpt:

NASA Technical Memorandum

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ISBN 13 :
Total Pages : 492 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 1994 with total page 492 pages. Available in PDF, EPUB and Kindle. Book excerpt: