Read Books Online and Download eBooks, EPub, PDF, Mobi, Kindle, Text Full Free.
Final Report On Heat Transfer Investigations In Supersonic Flow
Download Final Report On Heat Transfer Investigations In Supersonic Flow full books in PDF, epub, and Kindle. Read online Final Report On Heat Transfer Investigations In Supersonic Flow ebook anywhere anytime directly on your device. Fast Download speed and no annoying ads. We cannot guarantee that every ebooks is available!
Book Synopsis Final Report on Heat Transfer Investigations in Supersonic Flow by : John L. Harkness
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.
Book Synopsis Heat Transfer Investigations in Supersonic Flow by : John L. Harkness
Download or read book 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:
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:
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 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 An Experimental Investigation of Recovery Factors and Heat-transfer Coefficients for Supersonic Air Flow Over Flat Plates by : Robert Howard Shoulberg
Download or read book An Experimental Investigation of Recovery Factors and Heat-transfer Coefficients for Supersonic Air Flow Over Flat Plates written by Robert Howard Shoulberg and published by . This book was released on 1953 with total page 276 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis A Technique for Experimental Investigation of Heat Transfer from a Surface in Supersonic Flow at Large Surface-to-free-stream Temperature Ratios by : W. S. Bradfield
Download or read book A Technique for Experimental Investigation of Heat Transfer from a Surface in Supersonic Flow at Large Surface-to-free-stream Temperature Ratios written by W. S. Bradfield and published by . This book was released on 1958 with total page 22 pages. Available in PDF, EPUB and Kindle. Book excerpt: A description is given of an experimental technique for studying heat transfer at high temperatures. The direction of heat flux is from the surface to the boundary layer. Preliminary values of local convective and radiative heat transfer are reported. Some data are given on the deterioration of graphite surfaces coated with silicon nitride and silicon carbide.
Book Synopsis A Technique for Experimental Investigation of Heat Transfer from a Surface in Supersonic Flow at Large Surface-to-free-stream Temperature Ratios by : W. A. Bradfield
Download or read book A Technique for Experimental Investigation of Heat Transfer from a Surface in Supersonic Flow at Large Surface-to-free-stream Temperature Ratios written by W. A. Bradfield and published by . This book was released on 1958 with total page 33 pages. Available in PDF, EPUB and Kindle. Book excerpt: The experimental technique presented provides a surface of controlled moderately high temperature in a flow of homogeneous and chemically determined gas at high speeds. With this technique it is possible to make detailed temperature and power dissipation surveys over the controlled surface. Detailed Schlieren studies of processes occurring in the boundary layer at the heated surface under these circumstances may be obtained. It is possible to determine mass flux rates from small surface areas with comparatively good accuracy. The present laminar result shows reasonable correlation with the reference enthalpy method of predicting local values of heat flux but the correlation of this data with the theory must be substantiated by additional information. The investigation of heat flux in a region of a strong boundary layer shock wave interaction gives values approximately 4.5 times higher than those predicted by the laminar theory. Surface deterioration studies indicate that a silicon carbide coating on a graphite surface may be a practical inhibitor of surface deterioration at temperatures up to 3200 R in air.
Book Synopsis An Analytical Investigation of Turbulent Boundary Layer Heat Transfer Coefficients for Supersonic and Hypersonic Flow by : Jerome Persh
Download or read book An Analytical Investigation of Turbulent Boundary Layer Heat Transfer Coefficients for Supersonic and Hypersonic Flow written by Jerome Persh and published by . This book was released on 1955 with total page 0 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Experimental Investigation of Turbulent Boundary Layer Heat Transfer Rates on a Flat Plate in Low Mach Number Supersonic Flow with High Wall Cooling by : Kerry Gordon Geringer
Download or read book Experimental Investigation of Turbulent Boundary Layer Heat Transfer Rates on a Flat Plate in Low Mach Number Supersonic Flow with High Wall Cooling written by Kerry Gordon Geringer and published by . This book was released on 1973 with total page 168 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Experimental Investigation of the Effect of Boundary-layer Transition on the Average Heat Transfer to a Yawed Cylinder in Supersonic Flow by : Ivan E. Beckwith
Download or read book Experimental Investigation of the Effect of Boundary-layer Transition on the Average Heat Transfer to a Yawed Cylinder in Supersonic Flow written by Ivan E. Beckwith and published by . This book was released on 1956 with total page 38 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis An Analytical Investigation of Turbulent Boundary Layer Heat Transfer Coefficients for Supersonic and Hypersonic Flow by : JEROME. PERSH
Download or read book An Analytical Investigation of Turbulent Boundary Layer Heat Transfer Coefficients for Supersonic and Hypersonic Flow written by JEROME. PERSH and published by . This book was released on 1955 with total page 26 pages. Available in PDF, EPUB and Kindle. Book excerpt:
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 Experimental Investigation of Skin Friction and Heat Transfer at the Wall of a Supersonic Flow Channel by : Frederic Alan Gruenich
Download or read book Experimental Investigation of Skin Friction and Heat Transfer at the Wall of a Supersonic Flow Channel written by Frederic Alan Gruenich and published by . This book was released on 1962 with total page 88 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 24 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Theoretical Investigation of a Boundary Layer and Heat Transfer in a Supersonic Nozzle by : Edwin Snow Gallacher
Download or read book Theoretical Investigation of a Boundary Layer and Heat Transfer in a Supersonic Nozzle written by Edwin Snow Gallacher and published by . This book was released on 1950 with total page 214 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Theoretical Investigation of Laminar Heat Transfer on Yawed Infinite Cylinders in Supersonic Flow and a Comparison with Experimental Data by : Ivan E. Beckwith
Download or read book Theoretical Investigation of Laminar Heat Transfer on Yawed Infinite Cylinders in Supersonic Flow and a Comparison with Experimental Data written by Ivan E. Beckwith and published by . This book was released on 1955 with total page 46 pages. Available in PDF, EPUB and Kindle. Book excerpt: