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An Experimental Investigation Of Hypersonic Flow Around A Slender Cone
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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 Experimental Investigation of the Supersonic Flow Field about a Slender Cone at High Incidences by : C. Nebbeling
Download or read book Experimental Investigation of the Supersonic Flow Field about a Slender Cone at High Incidences written by C. Nebbeling and published by . This book was released on 1976 with total page 112 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis An Experimental Investigation of the Aerodynamic Characteristics of Slender Hypersonic Vehicles at High Angles of Attack by : Robert H. Feldhuhn
Download or read book An Experimental Investigation of the Aerodynamic Characteristics of Slender Hypersonic Vehicles at High Angles of Attack written by Robert H. Feldhuhn and published by . This book was released on 1968 with total page 148 pages. Available in PDF, EPUB and Kindle. Book excerpt: Pressure, heat transfer, force, flow field surveys and flow visualization measurements on an inclined cone were obtained in a wind tunnel at a nominal Mach number of 6. Force measurements were also obtained for a 2/3 power law body and two ducted-cone configurations.
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 An Experimental and Theoretical Investigation of the Pressure Distribution and Flow Fields of Blunted Cones at Hypersonic Mach Number by : Joseph W. Cleary
Download or read book An Experimental and Theoretical Investigation of the Pressure Distribution and Flow Fields of Blunted Cones at Hypersonic Mach Number written by Joseph W. Cleary and published by . This book was released on 1965 with total page 82 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis A Theoretical and Experimental Study of Hypersonic Flow Over Flared Bodies at Incidence by : John V. Rakich
Download or read book A Theoretical and Experimental Study of Hypersonic Flow Over Flared Bodies at Incidence written by John V. Rakich and published by . This book was released on 1966 with total page 60 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis An Experimental Investigation of the Flow Field Around an Inclined Sharp Cone in Hypersonic Flow by : Oscar L. George
Download or read book An Experimental Investigation of the Flow Field Around an Inclined Sharp Cone in Hypersonic Flow written by Oscar L. George and published by . This book was released on 1969 with total page 74 pages. Available in PDF, EPUB and Kindle. Book excerpt:
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 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 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 Hassell Street Press. This book was released on 2021-09-10 with total page 146 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.
Book Synopsis Experimental Investigation of Multiple-jet Liquid Injection Into Hypersonic Flow by : William F. Hinson
Download or read book Experimental Investigation of Multiple-jet Liquid Injection Into Hypersonic Flow written by William F. Hinson and published by . This book was released on 1970 with total page 50 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 Hypersonic Flow Over a Slender Cone with Gas Injection by : Hartley Hughes King
Download or read book Hypersonic Flow Over a Slender Cone with Gas Injection written by Hartley Hughes King and published by . This book was released on 1963 with total page 244 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 Hypersonic Flow Over a Slender Cone by : John Kliewer Wall
Download or read book Hypersonic Flow Over a Slender Cone written by John Kliewer Wall and published by . This book was released on 1957 with total page 202 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:
