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An Experimental Investigation Of Heat Transfer To Cones In Rarefied Hypersonic Flow
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Book Synopsis An Experimental Investigation of Heat Transfer to Cones in Rarefied Hypersonic Flow by : Carl T. Berry
Download or read book An Experimental Investigation of Heat Transfer to Cones in Rarefied Hypersonic Flow written by Carl T. Berry and published by . This book was released on 1971 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis An Experimental Investigation of Heat Transfer to Cones in Rarified Hypersonic Flow by : Carl T. Berry
Download or read book An Experimental Investigation of Heat Transfer to Cones in Rarified Hypersonic Flow written by Carl T. Berry and published by . This book was released on 1971 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis An Experimental Investigation of Hypersonic Flow Around a Slender Cone by : Edward M. Schmidt
Download or read book An Experimental Investigation of Hypersonic Flow Around a Slender Cone written by Edward M. Schmidt and published by . This book was released on 1967 with total page 44 pages. Available in PDF, EPUB and Kindle. Book excerpt: The paper presents the results of an experimental survey of the flow field around a sharp, 10 degree half angle cone. Tests were conducted at a free stream Mach number of 7.7 for a range of free stream Reynolds numbers of 110,000 to 171,000 per foot. Surface heat transfer data indicates that the cone boundary layer varies from laminar to fully developed turbulent over this Reynolds number range. The base pressure variation was also obtained throughout this range of Reynolds numbers; from this, the interrelation between the surface boundary layer properties and the base pressure is discussed. A series of tests were conducted in the near wake region at two different values of free stream Reynolds number, i.e., 330,000 and 1,650,000 per foot, corresponding to a completely laminar and fully developed turbulent surface boundary layer at the cone shoulder, respectively. The relationship between boundary layer properties and near wake properties is studied. (Author).
Book Synopsis An Experimental Investigation of Laminar Heat Transfer to Cones at Hypersonic Speeds by : Carl T. Berry
Download or read book An Experimental Investigation of Laminar Heat Transfer to Cones at Hypersonic Speeds written by Carl T. Berry and published by . This book was released on 1972 with total page 99 pages. Available in PDF, EPUB and Kindle. Book excerpt: The present study was an experimental investigation of the laminar surface heat transfer distribution about cones. The study was conducted in the Princeton University hypersonic nitrogen facility and covered a wide range of geometries and test conditions in an attempt to evaluate the numerical accuracy, theoretical modeling, and range of applicability of the several theories which are available. Cones, varying from 3 degrees to 30 degrees, with two nose bluntnesses, and lengths from one to eight inches were examined over a range of test conditions: Mach numbers from 16 to 25, and unit Reynolds numbers from 7,000 to 40,000 per inch. The detailed heat transfer distributions, covering the full range of 'nose dominated', 'merged', and 'weak interaction' regimes, were compared with several theoretical prediction techniques. A critical review of the modeling involved in the theories, as compared to the experiments, is presented. (Author).
Book Synopsis Hypersonic Rarefied Flow Over Sharp Slender Cones by : Marvin I. Kussoy
Download or read book Hypersonic Rarefied Flow Over Sharp Slender Cones written by Marvin I. Kussoy and published by . This book was released on 1972 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt: Drag, heat transfer, and number flux were measured on sharp cones in the near free, molecule flow regime, and the results were compared with available Monte Carlo calculations. In general, the calculations predicted the magnitude of the data; however, the heat transfer and drag increased with increasing Knudsen number at a faster rate than predicted. Also the drag coefficients measured for the slender cones at high Knudsen number were higher than predicted for free molecule flow. These disagreements between theory and experiment could possibly be attributed to the simplicity of the surface interaction laws assumed in the theory. Reynolds analogy factors obtained from the experimental measurements agreed with free-molecule values and also with that obtained by the Monte Carlo technique.
Book Synopsis Research on Heat Transfer in Spheres and Thin Cones in the Hypersonic Flow of a Rarefied Gas by : Yu V. Nikolskii
Download or read book Research on Heat Transfer in Spheres and Thin Cones in the Hypersonic Flow of a Rarefied Gas written by Yu V. Nikolskii and published by . This book was released on 1974 with total page 14 pages. Available in PDF, EPUB and Kindle. Book excerpt: The research sheds light on heat transfer in spheres and thin cones at a zero angle of attack. The investigations were conducted in a vacuum wind tunnel at Mach numbers M = 4.9-9.5, and Reynold numbers Re0 = 35-1 for spheres, and Re0 = 100-4 for cones; this corresponds to the transition range between free-molecular flow and the flow of a continuous medium. The procedure used was the measurement of the total heat flow under standard conditions with compensation of heat losses in a sting, and an independent measurement of the radiant heat flux. A comparison of the data with the results of the theoretical calculation was made.
Book Synopsis An Experimental Investigation of the Turbulent Boundary Layer in Supersonic Flow Around Unyawed Cones with Small Heat Transfer and Correlations with Two Dimensional Data by : Walter Samuel Bradfield
Download or read book An Experimental Investigation of the Turbulent Boundary Layer in Supersonic Flow Around Unyawed Cones with Small Heat Transfer and Correlations with Two Dimensional Data written by Walter Samuel Bradfield and published by . This book was released on 1957 with total page 344 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis An Experimental Investigation of Laminar Hypersonic Cavity Flows by : Kenneth M. Nicoll
Download or read book An Experimental Investigation of Laminar Hypersonic Cavity Flows written by Kenneth M. Nicoll and published by . This book was released on 1964 with total page 44 pages. Available in PDF, EPUB and Kindle. Book excerpt: An experimental investigation was made of the recovery factor and heat-transfer distributions on a set of cone-models incorporating annular cavities. This study is the second part of a two-part program. The first section contained measurements of the pressure distributions. The results show that the recovery factor in laminar, hypersonic cavity flow is almost constant within the cavity and downstream of reattachment, and is very close to the laminar attached-flow value. In the immediate vicinity of reattachment, the recovery factor is slightly higher than this value (less than 5%). The lowest values of the heat-transfer coefficient are found on the cavity floors, where a minimum of about 10 to 20% of the attached-flow value is reached. The highest values of the heat-transfer coefficient are in the immediate vicinity of reattachment. An average reattachment heattransfer coefficient of about three times the basic cone heat-transfer coefficient was measured on one cavity model. (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 Experimental Investigation of the Heat-transfer Rate to a Series of 20 Degree Cones of Various Surface Finishes at a Mach Number of 4.95 by : Jim J. Jones
Download or read book Experimental Investigation of the Heat-transfer Rate to a Series of 20 Degree Cones of Various Surface Finishes at a Mach Number of 4.95 written by Jim J. Jones and published by . This book was released on 1959 with total page 26 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Experimental Investigation of Heat-transfer Rate to Series of 20° Cones of Various Surface Finishes at Mach Number of 4.95 [with List of References] by :
Download or read book Experimental Investigation of Heat-transfer Rate to Series of 20° Cones of Various Surface Finishes at Mach Number of 4.95 [with List of References] written by and published by . This book was released on 1959 with total page 26 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis An Experimental Investigation of Hypersonic Flow Over Blunt Nosed Cones at a Mach Number of 5.8 by : Reginald M. Machell
Download or read book An Experimental Investigation of Hypersonic Flow Over Blunt Nosed Cones at a Mach Number of 5.8 written by Reginald M. Machell and published by . This book was released on 1956 with total page 0 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis An Experimental Investigation of Hypersonic Flow Over Blunt Nosed Cones at a Mach Number of 5.8 by : Reginald M. Machell
Download or read book An Experimental Investigation of Hypersonic Flow Over Blunt Nosed Cones at a Mach Number of 5.8 written by Reginald M. Machell and published by . This book was released on 1956 with total page 106 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis An Experimental Investigation of Hypersonic Flow Over Blunt Nosed Cones at a Mach Number of 5.8 by : William T. O'Bryant
Download or read book An Experimental Investigation of Hypersonic Flow Over Blunt Nosed Cones at a Mach Number of 5.8 written by William T. O'Bryant and published by . This book was released on 1956 with total page 0 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Heat Transfer from Right Circular Cones to a Rarefied Gas in Supersonic Flow by : Robert M. Drake
Download or read book Heat Transfer from Right Circular Cones to a Rarefied Gas in Supersonic Flow written by Robert M. Drake and published by . This book was released on 1952 with total page 26 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis An Experimental Investigation of Hypersonic Flow Over Blunt Nosed Cones at a Mach Number of 5.8 by : William T. O'Bryant
Download or read book An Experimental Investigation of Hypersonic Flow Over Blunt Nosed Cones at a Mach Number of 5.8 written by William T. O'Bryant and published by . This book was released on 1956 with total page 120 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis An Investigation of Laminar Heat Transfer to Slender Cones in the Hypersonic Shock Tunnel by : Charles E. Wittliff
Download or read book An Investigation of Laminar Heat Transfer to Slender Cones in the Hypersonic Shock Tunnel written by Charles E. Wittliff and published by . This book was released on 1961 with total page 82 pages. Available in PDF, EPUB and Kindle. Book excerpt: