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Author : Jean J. Ginoux
Publisher :
ISBN 13 :
Total Pages : 68 pages
Book Rating : 4.F/5 ( download)
Download or read book Supersonic Flow Over Flaps with Uniform Heat Transfer written by Jean J. Ginoux and published by . This book was released on 1966 with total page 68 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author :
Publisher :
ISBN 13 :
Total Pages : 704 pages
Book Rating : 4.:/5 (31 download)
Download or read book Scientific and Technical Aerospace Reports written by and published by . This book was released on 1995 with total page 704 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author :
Publisher : Academic Press
ISBN 13 : 0080575609
Total Pages : 591 pages
Book Rating : 4.0/5 (85 download)
Download or read book Advances in Heat Transfer written by and published by Academic Press. This book was released on 1970-07-31 with total page 591 pages. Available in PDF, EPUB and Kindle. Book excerpt: Advances in Heat Transfer
Author : John L. Harkness
Publisher :
ISBN 13 :
Total Pages : 58 pages
Book Rating : 4.:/5 (464 download)
Download or read book Final Report on Heat Transfer Investigations in Supersonic Flow written by John L. Harkness and published by . This book was released on 1958 with total page 58 pages. Available in PDF, EPUB and Kindle. Book excerpt: The major effort concerned with this project concerned the development of a small high stagnation temperature intermittant-flow supersonic wind tunnel and a description of this work and the resulting facility is presented. The development of an electrically heated shield temperature probe, for measurements of supersonic flow, is described and the results of an interference study, concerning total pressure probes in the boundary layer, are presented. Heat transfer measurements on a flat-plate model were accomplished and this ivestigation is described including a brief discussion of the test results. An analytical study concerning the temperature distribution through the turbulent boundary layer is also discussed. All of this work has been previously reported in considerable detail and specific references are given in each case.
Author : J. Don Gray
Publisher :
ISBN 13 :
Total Pages : 128 pages
Book Rating : 4.3/5 (91 download)
Download or read book Effects of Wall Cooling and Leading-edge Blunting on Ramp-induced, Laminar Flow Separations at Mach Numbers from 3 Through 6 written by J. Don Gray and published by . This book was released on 1972 with total page 128 pages. Available in PDF, EPUB and Kindle. Book excerpt: The effects of wall cooling and nose bluntness on laminar and transitional reattaching flows induced by a 9.5-degree ramp were investigated at Mach numbers from 3 through 6 measuring the longitudinal surface pressure and heat-transfer rate distributions, as well as the flow-field pressures, at several longitudinal stations. Reynolds number based on flat-plate length was varied from 0.25 to 1.0 million. The trend in the change in interaction length with Reynolds number increase indicated laminar reattachment at all test Reynolds numbers at M = 6 and transitional at the two higher Reynolds numbers at M = 3.
Author : Defense Documentation Center (U.S.)
Publisher :
ISBN 13 :
Total Pages : 784 pages
Book Rating : 4.:/5 (1 download)
Download or read book Technical Abstract Bulletin written by Defense Documentation Center (U.S.) and published by . This book was released on 1967 with total page 784 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : W. J. McCroskey
Publisher :
ISBN 13 :
Total Pages : 55 pages
Book Rating : 4.:/5 (123 download)
Download or read book Effect of a Stepwise Distribution of Heat Transfer on the Supersonic Flow Over a Flat Plate written by W. J. McCroskey and published by . This book was released on 1963 with total page 55 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Marcus O. Creager
Publisher :
ISBN 13 :
Total Pages : 54 pages
Book Rating : 4.:/5 (249 download)
Download or read book Effects of Leading-edge Blunting on the Local Heat Transfer and Pressure Distributions Over Flat Plates in Supersonic Flow written by Marcus O. Creager and published by . This book was released on 1957 with total page 54 pages. Available in PDF, EPUB and Kindle. Book excerpt: An investigation of the effect of leading-edge thickness on the flow over flat plates with square and cylindrical blunting was conducted at a Mach number of 4 and free-stream Reynolds numbers per inch of 2380 and 6600. Surface pressures were measured on a series of models whose leading-edge thicknesses ranged from 0.25 to 1 inch. Heat-transfer rates were measured from a flat plate which was blunted by a 1-inch-diameter cylindrical leading edge. All tests were performed with the instrumented surfaces at zero angle of sweep and zero angle of attack. For the test condition, the bow shock wave was detached and leading-edge shape had no effect on surface pressures aft of two leading-edge thicknesses. The surface pressures could be predicted by a combination of shock-wave boundary-layer interaction theory and blast wave theory. This combination applied equally well to similar data of other investigations. An empirical expression for local Reynolds number at the boundary-layer edge was found to correlate both the present data and data from other investigations covering a wide range of conditions. The local Reynolds number per inch was found to be lower than free-stream Reynolds number per inch, nearly constant for the test length, and to have negligible dependence on leading-edge bluntness. This reduction depends on the square root of the ratio of total pressures across the normal bow shock wave. The local Nusselt number was found to depend only on the local Reynolds number for the present tests, and is predicted by the familiar Pohlhausen flat-plate theory. As compared to the sharp condition, blunting the leading edge of flat plates, with consequent reduction of local total pressure, was found to increase the heat-transfer coefficients in the region where surface static pressures were high and to reduce the coefficients where the surface static pressures approached the free-stream value.
Author :
Publisher :
ISBN 13 :
Total Pages : 168 pages
Book Rating : 4.:/5 (31 download)
Download or read book U.S. Government Research & Development Reports written by and published by . This book was released on 1968 with total page 168 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : United States. National Aeronautics and Space Administration Scientific and Technical Information Division
Publisher :
ISBN 13 :
Total Pages : 966 pages
Book Rating : 4.F/5 ( download)
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:
Author : H.Y. Wong
Publisher :
ISBN 13 :
Total Pages : pages
Book Rating : 4.:/5 (11 download)
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:
Author : United States. National Aeronautics and Space Administration. Scientific and Technical Information Division
Publisher :
ISBN 13 :
Total Pages : 962 pages
Book Rating : 4.E/5 ( download)
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:
Author : United States. National Aeronautics and Space Administration. Scientific and Technical Information Division
Publisher :
ISBN 13 :
Total Pages : 956 pages
Book Rating : 4.:/5 (317 download)
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:
Author : Michael E. Tauber
Publisher :
ISBN 13 :
Total Pages : 44 pages
Book Rating : 4.:/5 (31 download)
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:
Author :
Publisher :
ISBN 13 :
Total Pages : 482 pages
Book Rating : 4.:/5 (319 download)
Download or read book NASA Technical Note written by and published by . This book was released on 1974 with total page 482 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : United States. Superintendent of Documents
Publisher :
ISBN 13 :
Total Pages : 1348 pages
Book Rating : 4.F/5 ( download)
Download or read book Monthly Catalog of United States Government Publications, Cumulative Index written by United States. Superintendent of Documents and published by . This book was released on 1970 with total page 1348 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author :
Publisher :
ISBN 13 :
Total Pages : 1388 pages
Book Rating : 4.:/5 (891 download)
Download or read book Monthly Catalog of United States Government Publications written by and published by . This book was released on with total page 1388 pages. Available in PDF, EPUB and Kindle. Book excerpt:
