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Author : Carl T. Berry
Publisher :
ISBN 13 :
Total Pages : pages
Book Rating : 4.:/5 (14 download)
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:
Author : Carl T. Berry
Publisher :
ISBN 13 :
Total Pages : pages
Book Rating : 4.:/5 (816 download)
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:
Author : Edward M. Schmidt
Publisher :
ISBN 13 :
Total Pages : 44 pages
Book Rating : 4.:/5 (227 download)
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).
Author : Carl T. Berry
Publisher :
ISBN 13 :
Total Pages : 99 pages
Book Rating : 4.:/5 (227 download)
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).
Author : Marvin I. Kussoy
Publisher :
ISBN 13 :
Total Pages : 36 pages
Book Rating : 4.:/5 (31 download)
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.
Author : Walter Samuel Bradfield
Publisher :
ISBN 13 :
Total Pages : 344 pages
Book Rating : 4.:/5 (319 download)
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:
Author : Michael C. Fischer
Publisher :
ISBN 13 :
Total Pages : 76 pages
Book Rating : 4.:/5 (31 download)
Download or read book An Experimental Investigation of Boundary-layer Transition on a 10 ̊half-angle Cone at Mach 6.9 written by Michael C. Fischer and published by . This book was released on 1970 with total page 76 pages. Available in PDF, EPUB and Kindle. Book excerpt: Boundary layer transition on nose cones at hypersonic speeds.
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 : Reginald M Machell
Publisher : Hassell Street Press
ISBN 13 : 9781013398810
Total Pages : 130 pages
Book Rating : 4.3/5 (988 download)
Download or read book An Experimental Investigation by Hypersonic Flow Over Blunt Nosed Cones at a Mach Number of 5.8. written by Reginald M Machell and published by Hassell Street Press. This book was released on 2021-09-09 with total page 130 pages. Available in PDF, EPUB and Kindle. Book excerpt: This work has been selected by scholars as being culturally important and is part of the knowledge base of civilization as we know it. This work is in the public domain in the United States of America, and possibly other nations. Within the United States, you may freely copy and distribute this work, as no entity (individual or corporate) has a copyright on the body of the work. Scholars believe, and we concur, that this work is important enough to be preserved, reproduced, and made generally available to the public. To ensure a quality reading experience, this work has been proofread and republished using a format that seamlessly blends the original graphical elements with text in an easy-to-read typeface. We appreciate your support of the preservation process, and thank you for being an important part of keeping this knowledge alive and relevant.
Author : Reginald M. Machell
Publisher :
ISBN 13 :
Total Pages : 0 pages
Book Rating : 4.:/5 (437 download)
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:
Author : Marvin I. Kussoy
Publisher :
ISBN 13 :
Total Pages : 20 pages
Book Rating : 4.:/5 (31 download)
Download or read book Hypersonic Viscous Drag on Cones in Rarefied Flow written by Marvin I. Kussoy and published by . This book was released on 1967 with total page 20 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Yu V. Nikolskii
Publisher :
ISBN 13 :
Total Pages : 14 pages
Book Rating : 4.:/5 (227 download)
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.
Author : William T. O'Bryant
Publisher :
ISBN 13 :
Total Pages : 0 pages
Book Rating : 4.:/5 (437 download)
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:
Author : Kenneth M. Nicoll
Publisher :
ISBN 13 :
Total Pages : 44 pages
Book Rating : 4.:/5 (41 download)
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).
Author : William T. O'Bryant
Publisher :
ISBN 13 :
Total Pages : 120 pages
Book Rating : 4.:/5 (437 download)
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:
Author : Charles E. Wittliff
Publisher :
ISBN 13 :
Total Pages : 82 pages
Book Rating : 4.E/5 ( download)
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:
Author : Jim J. Jones
Publisher :
ISBN 13 :
Total Pages : 26 pages
Book Rating : 4.:/5 (11 download)
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:
