Download or read book Heat Transfer to Flat Plate in High temperature Rarefied Ultra high Mach Number Flow written by H. T. Nagamatsu and published by . This book was released on 1961 with total page 50 pages. Available in PDF, EPUB and Kindle. Book excerpt: An investigation was conducted in a hypersonic shock tunnel to determine the local heat transfer rates for a sharp leading edge flat plate. The free stream Mach number range was 7.95 to 25.l with stagnation temperatures of approximately 2550 and 6500 R. For these temperature and Mach number conditions, the strong interaction parameter varied from 2.35 to 826. The corresponding Knudsen numbers, based on the ratio of the free stream mean free path and the leading edge thickness, varied from 0.38 to 85.5. The sputtered platinum heat gages were dynamically calibrated by passing a moderate strength shock wave across the gages and observing the change in resistance due to a step function temperature rise. By this method the gage characteristics were determined for the same pressure rises encountered in the test section.
Download or read book Rarefied High temperature Ultrahigh Mach Number Slip Flow Over a Sharp Flat Plate written by H. T. NAGAMATSU and published by . This book was released on 1963 with total page 39 pages. Available in PDF, EPUB and Kindle. Book excerpt: An investigation was conducted in a hypersonic shock tunnel to determine the induced pressures and the local heat transfer rates for a flat plate with sharp leading edge. The free stream Mach number range was 7.95 to 25.1 with stagnation temperatures of approximately 2300 and 7000 R. For these temperatures and Mach number conditions, the strong interaction parameter, varied from 2.35 to 826 and the corresponding Knudsen numbers, based on the ratio of the free stream mean free path and the leading edge thickness, varied from 0.4 to 86. For free stream Mach numbers greater than 10, Knudsen numbers of approximately unity, and perfect gas conditions, the observed experimental induced pressures varied as the square root of the strong interaction parameter and the local heat transfer rates varied as the cube root of the strong interaction parameter to the fourth power as predicted by the noninsulated flat plate theory of Li and Nagamatsu. When the Knudsen number and the Mach number are much greater than 1, the leading edge slip phenomenon drastically reduced both the induced pressures and local heat transfer rates as compared to the theoretical values predicted with no slip at the surface. Schlieren photographs indicate the presence of slip flow at the sharp leading edge in that the formation of the strong shock wave and the boundary layer was delayed. (Author).
Download or read book Heat Transfer on a Flat Plate in Continuum to Rarefied Hypersonic Flows at Mach Numbers of 19 2 and 25 4 written by Henry T. Nagamatsu and published by . This book was released on 1970 with total page 68 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Technical Papers written by and published by . This book was released on 1964 with total page 286 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Transition in Turbines written by and published by . This book was released on 1985 with total page 238 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book U S Government Research Reports written by and published by . This book was released on 1964 with total page 1076 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Heat Mass and Momentum Transfer for Flow Over a Flat Plate with Blowing Or Suction written by H. S. Mickley and published by . This book was released on 1954 with total page 166 pages. Available in PDF, EPUB and Kindle. Book excerpt: The effect on the boundary layer of sucking or blowing air through a porous flat plate into or out of a main air stream flowing parallel to the plate was studied theoretically and experimentally.
Download or read book The High Temperature Aspects of Hypersonic Flow written by Wilbur C. Nelson and published by Elsevier. This book was released on 2014-12-02 with total page 801 pages. Available in PDF, EPUB and Kindle. Book excerpt: The High Temperature Aspects of Hypersonic Flow is a record of the proceedings of the AGARD-NATO Specialists' Meeting, held at the Technical Centre for Experimental Aerodynamics, Rhode-Saint-Genese, Belgium in April 1962. The book contains the papers presented during the meeting that tackled a broad range of topics in the aspects of hypersonic flow. The subjects covered during the meeting include pressure measurements, interference effects, the use of wind tunnels in aircraft development testing, high temperature gas characteristics, boundary layer research, stability and control and the use of rocket vehicles in flight research. Aerospace engineers and aeronautical engineers will find the book invaluable.
Download or read book Heat transfer Measurements at a Mach Number of 2 in the Turbulent Boundary Layer on a Flat Plate Having a Stepwise Temperature Distribution written by Raul J. Conti and published by . This book was released on 1959 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Heat transfer Measurements at a Mach Number of 2 in the Turbulent Boundary Layer on a Flat Plate Having a Stepwise Temperature Distribution written by Raul Jorge Conti and published by . This book was released on 1959 with total page 32 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Scientific and Technical Aerospace Reports written by and published by . This book was released on 1992 with total page 292 pages. Available in PDF, EPUB and Kindle. Book excerpt:
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:
Download or read book The Effect of an Arbitrary Surface temperature Variation Along a Flat Plate on the Convective Heat Transfer in an Incompressible Turbulent Boundary Layer written by Morris W. Rubesin and published by . This book was released on 1951 with total page 46 pages. Available in PDF, EPUB and Kindle. Book excerpt: An analysis was performed to determine the effects on the rates of convective heat transfer produced by arbitrary variations of the surface temperature with distance along a flat plate. The analysis was confined to the case of a low-speed turbulent boundary layer on a flat plate oriented parallel to the free-stream velocity. It was found that a continuously variable surface temperature has, in general, a smaller effect on the local convective heat transfer than does a surface-temperature discontinuity.
Download or read book Jet Propulsion written by and published by . This book was released on 1962 with total page 1024 pages. Available in PDF, EPUB and Kindle. Book excerpt: Beginning Oct. 1959 some issues include "Russian supplement."
Download or read book Analysis of Turbulent Flow and Heat Transfer on Flat Plate at High Mach Numbers with Variable Fluid Properties with List of References written by and published by . This book was released on 1959 with total page 33 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Air Force Research Resum s written by and published by . This book was released on with total page 592 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Factors Determining the Performance of Indexing Systems written by Cyril W. Cleverdon and published by . This book was released on 1966 with total page 266 pages. Available in PDF, EPUB and Kindle. Book excerpt:
