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Investigation Of Heat Transfer In Base Type Supersonic Laminar And Transitional Separated Flows
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Book Synopsis Investigation of Heat Transfer in Base Type Supersonic Laminar and Transitional Separated Flows by : Josef Rom
Download or read book Investigation of Heat Transfer in Base Type Supersonic Laminar and Transitional Separated Flows written by Josef Rom and published by . This book was released on 1970 with total page 48 pages. Available in PDF, EPUB and Kindle. Book excerpt: Heat transfer rate distributions were measured in the separated regions of a two-dimensional backward facing step, an axially symmetric backward facing step, a blunt two-dimensional base, a sharp protruding two-dimensional leading edge and in the leading edge bubble over the surface of a flat nosed two-dimensional model. The results of these measurements are compared with measurements of heat transfer rates in various base type separated flows obtained in various wind tunnels and to a calculation of heat transfer behind a backward facing step based on the integral method. In most of these investigations a high peak in the heat transfer rate is found to occur in the reattachment zone. Maximum heat transfer rate values of up to 10 times the flat plate heat transfer rate are reported in various investigations. An inverse relation between the value of the peak heat transfer rate and the distance between the separation point to the position of the maximum heating in the reattachment zone is shown to exist. (Author).
Book Synopsis Scientific Report No. 1 by : Josef Rom
Download or read book Scientific Report No. 1 written by Josef Rom and published by . This book was released on 1970 with total page 44 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Investigation of Heat Transfer in Base Type Suprsonic Laminar and Transitional Separated Flows by : Josef Rom
Download or read book Investigation of Heat Transfer in Base Type Suprsonic Laminar and Transitional Separated Flows written by Josef Rom and published by . This book was released on 1970 with total page 44 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis An Investigation of Laminar, Transitional and Turbulent Heat Transfer on Blunt-nosed Bodies in Hypersonic Flow by : Robert J. Cresci
Download or read book An Investigation of Laminar, Transitional and Turbulent Heat Transfer on Blunt-nosed Bodies in Hypersonic Flow written by Robert J. Cresci and published by . This book was released on 1959 with total page 60 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Investigations of Near Wake Flow Field and Heat Transfer on Two Dimensional and Axially Symmetric Bodies at Supersonic Speeds by : Josef Rom
Download or read book Investigations of Near Wake Flow Field and Heat Transfer on Two Dimensional and Axially Symmetric Bodies at Supersonic Speeds written by Josef Rom and published by . This book was released on 1969 with total page 41 pages. Available in PDF, EPUB and Kindle. Book excerpt: Laminar and transitional heat transfer rates were measured in various base type separated flows in the shock tube. The application of the hot wire technique for measurements of the flow field in the supersonic near wake is studied. It is shown that using the measurements of a hot wire probe and a total pressure probe enable the determination of all the required physical parameters of the dissipative flow field in the near wake. The flow field behind a blunt two dimensional base model is measured. Mach number and total temperature profiles are determined and the various zones in the flow field are identified. (Author).
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:
Book Synopsis Preliminary Report on a Study of Separated Flows in Supersonic and Subsonic Streams by : Dean R. Chapman
Download or read book Preliminary Report on a Study of Separated Flows in Supersonic and Subsonic Streams written by Dean R. Chapman and published by . This book was released on 1956 with total page 24 pages. Available in PDF, EPUB and Kindle. Book excerpt: Some results are described of fundamental research conducted on various flow separation phenomena in two-dimensional streams. Experimental and theoretical results are described for the pressure rise across a reattachment region, and for the Reynolds number dependence of the pressure rise to a separation point. Observations are made throughout of the location of transition relative to reattachment and to separation, since this relative location turned out to be the dominant variable investigated.
Book Synopsis Supersonic Flow Over Flaps with Uniform Heat Transfer by : Jean J. Ginoux
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:
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 704 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Laminar and Transitional Heat Transfer in the Two-dimensional Separated Flow Behind a Sharp Protruding Leading Edge by : Josef Rom
Download or read book Laminar and Transitional Heat Transfer in the Two-dimensional Separated Flow Behind a Sharp Protruding Leading Edge written by Josef Rom and published by . This book was released on 1967 with total page 32 pages. Available in PDF, EPUB and Kindle. Book excerpt: Heat transfer rates are measured in the separated flow region behind the two-dimensional sharp protruding leading edge step model (boundary layer thickness is zero at the separation point) in the high enthalpy laminar near subsonic and supersonic flow in the shock tube. The measurements are carried out in a shock Mach number range from 2.3 to 10, and a corresponding flow Mach number range from 0.5 to 2.62. The Reynolds number, which is based on the height of the leading edge above the flat plate where the heat transfer rates are measured, varies from 300 to 17,000, and the local Reynolds number on the plate varies from 700 to 290,000. The results are correlated in terms of the non dimensional parameters of Nusselt number as a function of the Mach and Reynolds numbers and stagnation to wall enthalpy ratio. The variations of local, average and maximum heat transfer rates are presented. (Author).
Book Synopsis OAR Cumulative Index of Research Results by : United States. Air Force. Office of Aerospace Research
Download or read book OAR Cumulative Index of Research Results written by United States. Air Force. Office of Aerospace Research and published by . This book was released on 1963 with total page 550 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Government Reports Annual Index by :
Download or read book Government Reports Annual Index written by and published by . This book was released on 1988 with total page 1424 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis U.S. Government Research & Development Reports by :
Download or read book U.S. Government Research & Development Reports written by and published by . This book was released on 1970 with total page 224 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis A Collection of Technical Papers by :
Download or read book A Collection of Technical Papers written by and published by . This book was released on 1970 with total page 888 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis An Investigation of Laminar, Transitional and Turbulent Heat Transfer on Blunt-nosed Bodies in Hypersonic Flow by : Robert J. Cresci
Download or read book An Investigation of Laminar, Transitional and Turbulent Heat Transfer on Blunt-nosed Bodies in Hypersonic Flow written by Robert J. Cresci and published by . This book was released on 1959 with total page 0 pages. Available in PDF, EPUB and Kindle. Book excerpt:
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:
Book Synopsis An Experimental Investigation of Heat Transfer Effects on Boundary Layer Separation in Supersonic Flow by : G. E. Gadd
Download or read book An Experimental Investigation of Heat Transfer Effects on Boundary Layer Separation in Supersonic Flow written by G. E. Gadd and published by . This book was released on 1956 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
