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An Experimental Investigation Of Heat Transfer Rates On A Blunt Body In Hypersonic Flow
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Book Synopsis An Experimental Investigation of Heat Transfer Rates on a Blunt Body in Hypersonic Flow by : Homer K. Richards
Download or read book An Experimental Investigation of Heat Transfer Rates on a Blunt Body in Hypersonic Flow written by Homer K. Richards and published by . This book was released on 1957 with total page 66 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis An Experimental Investigation of Heat Transfer Rates on a Blunt Body in Hypersonic Flow by : Homer K. Richards
Download or read book An Experimental Investigation of Heat Transfer Rates on a Blunt Body in Hypersonic Flow written by Homer K. Richards and published by . This book was released on 1957 with total page 0 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Experimental and Numerical Study of Heat Transfer on a Blunt Body in Dusty Hypersonic Flow by : E. B. Vasilevskii
Download or read book Experimental and Numerical Study of Heat Transfer on a Blunt Body in Dusty Hypersonic Flow written by E. B. Vasilevskii and published by . This book was released on 1999 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis An Experimental Study of the Pressure and Heat-transfer Distribution on a 70° Sweep Slab Delta Wing in Hypersonic Flow by : Mitchel H. Bertram
Download or read book An Experimental Study of the Pressure and Heat-transfer Distribution on a 70° Sweep Slab Delta Wing in Hypersonic Flow written by Mitchel H. Bertram and published by . This book was released on 1963 with total page 136 pages. Available in PDF, EPUB and Kindle. Book excerpt: Results are presented for a study of the pressure and heat-transfer distributions and force characteristics of slab delta wings of 70° sweep at Mach numbers of 6.8 and 9.6 in air and 18 in helium. The wings had cylindrical leading edges and were tested with two different noses. One was sharp in plan view and the other was a tangent sphere with the same diameter as the cylindrical leading edge. Simple approaches to predicting the heat transfer are shown to be successful if the flow pattern peculiar to the angle-of-attack range under consideration is taken into account.
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 Aerodynamic Heating in Supersonic and Hypersonic Flows by : Mostafa Barzegar Gerdroodbary
Download or read book Aerodynamic Heating in Supersonic and Hypersonic Flows written by Mostafa Barzegar Gerdroodbary and published by Elsevier. This book was released on 2022-10-11 with total page 248 pages. Available in PDF, EPUB and Kindle. Book excerpt: Aerodynamic Heating in Supersonic and Hypersonic Flows: Advanced Techniques for Drag and Aero-heating Reduction explores the pros and cons of different heat reduction techniques on other characteristics of hypersonic vehicles. The book begins with an introduction of flow feature around the forebody of space vehicles and explains the main parameters on drag force and heat production in this region. The text then discusses the impact of severe heat production on the nose of hypervelocity vehicles, different reduction techniques for aerodynamic heating, and current practical applications for forebody shock control devices. Delivers valuable insight for aerospace engineers, postgraduate students, and researchers. Presents computational results of different cooling systems for drag and heat reduction around nose cones Explains mechanisms of drag reduction via mechanical, fluidic, and thermal systems Provides comprehensive details about the aerodynamics of space vehicles and the different shock features in the forebody of super/hypersonic vehicles Describes how numerical simulations are used for the development of the current design of forebody of super/hypersonic vehicles
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 Experimental Methods of Shock Wave Research by : Ozer Igra
Download or read book Experimental Methods of Shock Wave Research written by Ozer Igra and published by Springer. This book was released on 2015-10-31 with total page 480 pages. Available in PDF, EPUB and Kindle. Book excerpt: This comprehensive and carefully edited volume presents a variety of experimental methods used in Shock Waves research. In 14 self contained chapters this 9th volume of the “Shock Wave Science and Technology Reference Library” presents the experimental methods used in Shock Tubes, Shock Tunnels and Expansion Tubes facilities. Also described is their set-up and operation. The uses of an arc heated wind tunnel and a gun tunnel are also contained in this volume. Whenever possible, in addition to the technical description some typical scientific results obtained using such facilities are described. Additionally, this authoritative book includes techniques for measuring physical properties of blast waves and laser generated shock waves. Information about active shock wave laboratories at different locations around the world that are not described in the chapters herein is given in the Appendix, making this book useful for every researcher involved in shock/blast wave phenomena.
Book Synopsis Preliminary Experimental Investigation of the Flow about a Blunt Body with Flow-separation Spikes at M00 by : Victor Zakkay
Download or read book Preliminary Experimental Investigation of the Flow about a Blunt Body with Flow-separation Spikes at M00 written by Victor Zakkay and published by . This book was released on 1961 with total page 15 pages. Available in PDF, EPUB and Kindle. Book excerpt: The pressure and heat transfer distribution about a hemispherically-capped cone having a cone half angle of 50 degrees, and a bluntness ratio of R/Ro=0.667, equipped with flow-separation spikes, is presented in this report. The measurements wer made at a Mach number of 7.9.
Book Synopsis An Experimental Study of the Effect of Mass Injection at the Stagnation Point of a Blunt Body by : Howard K. McMahon
Download or read book An Experimental Study of the Effect of Mass Injection at the Stagnation Point of a Blunt Body written by Howard K. McMahon and published by . This book was released on 1958 with total page 182 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Experimental Heat Transfer to Blunt Axisymmetric Bodies Near the Limit of Continuum Flow by : J. Leith Potter
Download or read book Experimental Heat Transfer to Blunt Axisymmetric Bodies Near the Limit of Continuum Flow written by J. Leith Potter and published by . This book was released on 1962 with total page 26 pages. Available in PDF, EPUB and Kindle. Book excerpt: Measurements of average heat-transfer rates to blunt-nosed, axisymmetric, cold-walled bodies in a low-density, hypervelocity wind tunnel are given. Stream density was such that Reynolds and Knudsen numbers, based on nose radius and conditions immediately behind the bow shock, varied from 5 to 20 and 0.11 to 0.056, respectively. Thus, scaling on the basis of Knudsen number, these conditions may be said to simulate a body of one-foot nose radius at as much as 315,500-ft altitude. Heat-transfer rates are discussed in relation to the flow model successfully used in the past for studies of flows of high Reynolds number. In this context, it was found that measured heat-transfer rates to hemispheres below shock-layer Reynolds numbers of 20 exhibited a decreasing nondimensionalized rate relative to that estimated by methods appropriate to high Reynolds number conditions. This behavior is in accord with various applicable theories. Rates for the flat-faced bodies showed no tendency to decrease, and they were somewhat higher than predicted by theories for high Reynolds numbers.
Book Synopsis Effects of a Magnetic Field on the Hypervelocity Flow about a Blunt Body by : Richard W. Ziemer
Download or read book Effects of a Magnetic Field on the Hypervelocity Flow about a Blunt Body written by Richard W. Ziemer and published by . This book was released on 1958 with total page 52 pages. Available in PDF, EPUB and Kindle. Book excerpt: An experimental investigation was made of the effect of an applied magnetic field on the bow shock of a blunt body in hypervelocity air flow. Quantitative measurements of the stand-off distance were made in a three-inch electromagnetic shock tube with free-stream velocities up to 22,000 feet per second. The test body was a hemispherical cylinder containing a coaxial pulsed magnet coil in the nose which produced field strengths at the stagnation point of up to 40 kilogauss. The application of the magnetic field displaced the bow shock upstream and the stand-off distance increased by a factor of 7.5 for the condition, nondimensional parameter = 69. The experimental results were compared with theory and good agreement was obtained within the range of experimental conditions. (Author).
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 Experimental Investigation of Blunt Base Heat Transfer in an Axisymmetric Turbulent Supersonic Separated Flow by : L. S. Fletcher
Download or read book Experimental Investigation of Blunt Base Heat Transfer in an Axisymmetric Turbulent Supersonic Separated Flow written by L. S. Fletcher and published by . This book was released on 1969 with total page 49 pages. Available in PDF, EPUB and Kindle. Book excerpt: The heat transfer from a blunt base immersed in an axisymmetric turbulent supersonic separated flow was experimentally measured. The investigation was conducted at a Mach number and Reynolds number per foot of 3.88 and 16,700,000, respectively. Experimental heat transfer data, determined by a transient heat transfer technique, were obtained for both heated and cooled base conditions. A series of three models were used, permitting the measurement of an average value of base heat transfer, as well as the angular and radial variations. The experimental data obtained in the investigation were compared with published experimental data and with recently published correlating parameters for both base heating and base cooling. (Author).
Book Synopsis Technical Publications Announcements with Indexes by : United States. National Aeronautics and Space Administration
Download or read book Technical Publications Announcements with Indexes written by United States. National Aeronautics and Space Administration and published by . This book was released on 1962 with total page 1556 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis U.S. Government Research Reports by :
Download or read book U.S. Government Research Reports written by and published by . This book was released on 1964 with total page 286 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Technical Abstract Bulletin written by and published by . This book was released on with total page 912 pages. Available in PDF, EPUB and Kindle. Book excerpt:
