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A Study Of Laminar Heat Transfer To Spherically Blunted Cones And Hemisphere Cylinders At Hypersonic Conditions
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Book Synopsis A Study of Laminar Heat Transfer to Spherically Blunted Cones and Hemisphere-cylinders at Hypersonic Conditions by : B. J. Griffith
Download or read book A Study of Laminar Heat Transfer to Spherically Blunted Cones and Hemisphere-cylinders at Hypersonic Conditions written by B. J. Griffith and published by . This book was released on 1963 with total page 44 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Investigation of the Laminar Aerodynamic Heat-transfer Characteristics of a Hemisphere-cylinder in the Langley 11-inch Hypersonic Tunnel at a Mach Number of 6.8 by : Davis H. Crawford
Download or read book Investigation of the Laminar Aerodynamic Heat-transfer Characteristics of a Hemisphere-cylinder in the Langley 11-inch Hypersonic Tunnel at a Mach Number of 6.8 written by Davis H. Crawford and published by . This book was released on 1956 with total page 680 pages. Available in PDF, EPUB and Kindle. Book excerpt: At the stagnation point, the theory of Sibulkin, using the diameter and conditions behind the normal shock, was in good agreement with the experiment when the velocity graident at the stagnation opint appropriate to the free-stream Mach number was used.
Book Synopsis Laminar Heat Transfer to Spherically Blunted Cones at Hypersonic Conditions by : William Law
Download or read book Laminar Heat Transfer to Spherically Blunted Cones at Hypersonic Conditions written by William Law and published by . This book was released on 1964 with total page 54 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Laminar Heat Transfer on Sharp and Blunt Ten-degree Cones in Conical and Parallel Low-density Flow by : David E. Boylan
Download or read book Laminar Heat Transfer on Sharp and Blunt Ten-degree Cones in Conical and Parallel Low-density Flow written by David E. Boylan and published by . This book was released on 1973 with total page 68 pages. Available in PDF, EPUB and Kindle. Book excerpt: The report presents heat-transfer-rate measurements on sharp and blunt 10-deg half-angle cones at angles of attack between -9 and +10 deg in a low-density, hypersonic wind tunnel. Circumferential and longitudinal distributions are presented for cold wall conditions for a range at Mach and Reynolds numbers. The effect of source-like flows was studied by utilizing both conical and contoured expansion nozzles with the same free-stream similarity parameters and model wall temperatures. Comparisons are made with previously published experimental and theoretical results. (Author).
Book Synopsis Laminar Heat-transfer and Pressure Measurements at a Mach Number of 6 on a Sharp and Blunt 15° Half-angle Cones at Angles of Attack Up to 90° by : Raul Jorge Conti
Download or read book Laminar Heat-transfer and Pressure Measurements at a Mach Number of 6 on a Sharp and Blunt 15° Half-angle Cones at Angles of Attack Up to 90° written by Raul Jorge Conti and published by . This book was released on 1961 with total page 38 pages. Available in PDF, EPUB and Kindle. Book excerpt: Two circulation conical configurations having 15° half-angles were tested in laminar boundary layer at a Mach number of 6 and angles of attack up to 90°. One cone had a sharp nose and a fineness ratio of 1.87 and the other had a spherically blunted nose with a bluntness ratio of 0.1428 and a fineness ratio of 1.66. Pressure measurements and schlieren pictures of the flow showed that near-conical flow existed above 70° high pressure areas were present near the base and the bow shock wave was considerably curved.
Book Synopsis A Series Solution to the Laminar Heat Transfer Problem at Hypersonic Speeds by : Hung-Ta Ho
Download or read book A Series Solution to the Laminar Heat Transfer Problem at Hypersonic Speeds written by Hung-Ta Ho and published by . This book was released on 1958 with total page 90 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Heat Transfer to a Hemispherically Blunted 9 Deg Half-angle Cone Cylinder at Hypersonic Free Flight Mach Numbers Up to 20.4 by :
Download or read book Heat Transfer to a Hemispherically Blunted 9 Deg Half-angle Cone Cylinder at Hypersonic Free Flight Mach Numbers Up to 20.4 written by and published by . This book was released on 1964 with total page 46 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:
Book Synopsis Comparisons of Experimental and Theoretical Heat Transfer to a Yawed Sphere-cone Model at Supersonic Speeds by : Lionel Pasiuk
Download or read book Comparisons of Experimental and Theoretical Heat Transfer to a Yawed Sphere-cone Model at Supersonic Speeds written by Lionel Pasiuk and published by . This book was released on 1964 with total page 72 pages. Available in PDF, EPUB and Kindle. Book excerpt: Theoretical laminar heat transfer rates to a sphere-cone model at angles of yaw up to 18 degrees are compared with wind tunnel data measured at Mach numbers of 3.2 and 4.8. Two methods of heat transfer prediction have been chosen--the methods of Beckwith and VaglioLaurin. These require that the inviscid streamline pattern on the surface of the yawed spherecone model be known. These steamlines have been calculated from measured surface pressure distributions. The theory of Beckwith agrees reasonably well with the experimental data.
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 Convective Heat-transfer Rates on a Blunted 110° Cone with Hemispherical Afterbody at Hypersonic Speeds by : David A. Stewart
Download or read book Convective Heat-transfer Rates on a Blunted 110° Cone with Hemispherical Afterbody at Hypersonic Speeds written by David A. Stewart and published by . This book was released on 1971 with total page 28 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book NASA Technical Note written by and published by . This book was released on 1967 with total page 970 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Hypersonic Laminar Heat Transfer and Boundary Layer Transition on Sharp and Blunted Cones by : N. B. Wood
Download or read book Hypersonic Laminar Heat Transfer and Boundary Layer Transition on Sharp and Blunted Cones written by N. B. Wood and published by . This book was released on 1968 with total page 41 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Heat-transfer and Pressure Distributions on Spherically Blunted 25 ̊half-angle Cone at Mach 8 and Angles of Attack Up to 90 ̊ by : Dennis M. Bushnell
Download or read book Heat-transfer and Pressure Distributions on Spherically Blunted 25 ̊half-angle Cone at Mach 8 and Angles of Attack Up to 90 ̊ written by Dennis M. Bushnell and published by . This book was released on 1968 with total page 40 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Measurements of Hypersonic Turbulent Heat Transfer on a Highly Cooled Cone by : Donald M. Wilson
Download or read book Measurements of Hypersonic Turbulent Heat Transfer on a Highly Cooled Cone written by Donald M. Wilson and published by . This book was released on 1967 with total page 94 pages. Available in PDF, EPUB and Kindle. Book excerpt: Turbulent boundary layer heat transfer rates were measured on a thin-walled slender cone at a free-stream Mach number of 5.0. Wall to stagnation temperature ratios from 0.15 to 0.40 were obtained by pre-cooling the model using liquid nitrogen. Tests at a wide range of Reynolds numbers were conducted by varying the tunnel supply pressure; thus providing data for both laminar and mixed laminar-turbulent types of boundary layers. The experimental results obtained were compared with existing theories which predict convective heat transfer coefficients. These comparisons indicate that the data corresponding to a 760R supply temperature verify the predictions of Winkler and Cha; however, data acquired at a supply temperature of 1160R substantiate the predictions of Spalding and Chi. (Author).
Book Synopsis Heat Transfer and Temperature Distribution in a Hemispherical Nose Cone in Hypersonic Flow by : S. V. Nardo
Download or read book Heat Transfer and Temperature Distribution in a Hemispherical Nose Cone in Hypersonic Flow written by S. V. Nardo and published by . This book was released on 1962 with total page 72 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 1973 with total page 1040 pages. Available in PDF, EPUB and Kindle. Book excerpt: Lists citations with abstracts for aerospace related reports obtained from world wide sources and announces documents that have recently been entered into the NASA Scientific and Technical Information Database.
