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Heat Transfer And Pressure Distributions On Re Entry Nose Shapes In The Vki Longshot Hypersonic Tunnel
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Book Synopsis Heat Transfer and Pressure Distributions on Re-Entry Nose Shapes in the VKI Longshot Hypersonic Tunnel by :
Download or read book Heat Transfer and Pressure Distributions on Re-Entry Nose Shapes in the VKI Longshot Hypersonic Tunnel written by and published by . This book was released on 1971 with total page 89 pages. Available in PDF, EPUB and Kindle. Book excerpt: Heat transfer and pressure distributions have been made on five vehicle nose shapes in the VKI Longshot free piston wind tunnel at M=15 and 20. The flow parameters achieved closely simulate aerodynamic re-entry conditions. The models used in the study were 50-58 degree biconic configuration, with sharp-and blunt-nosed versions and a sharp-nosed version with a machined roughness, and a hemisphere configuration with a smooth and a sand-blast rough surface. These configurations resemble the stable shapes of turbulent and laminar ablating nose cones. Preliminary comparisons have been made with the state-of-the art engineering predictions. Some discussion about the state of the boundary layer is included.
Book Synopsis Hypersonic Heat Transfer Measurements on Reentry Vehicle Surfaces at High Reynolds Number by : Bryan E. Richards
Download or read book Hypersonic Heat Transfer Measurements on Reentry Vehicle Surfaces at High Reynolds Number written by Bryan E. Richards and published by . This book was released on 1973 with total page 50 pages. Available in PDF, EPUB and Kindle. Book excerpt: Heat transfer rates using calorimeter sensors, and pressures using variable reluctance diaphragm transducers, have been measured on five model shapes at Mach numbers of 15 and 20 and over a unit Reynolds number range of 2 million to 7 million per foot. Two basic shapes, a hemisphere and a half-angle biconic configuration with and without nose bluntness, were tested with different surface roughness. The results are reported and discussed. (Modified author abstract).
Book Synopsis Hypersonic Heat Transfer Measurements on Re-entry Vehivle Surfaces at High Reynolds Number by : Bryan E. Richards
Download or read book Hypersonic Heat Transfer Measurements on Re-entry Vehivle Surfaces at High Reynolds Number written by Bryan E. Richards and published by . This book was released on 1973 with total page 90 pages. Available in PDF, EPUB and Kindle. Book excerpt: Heat transfer rates using calorimeter sensors, and pressures using variable reluctance diaphragm transducers, have been measured on five model shapes at Mach numbers of 15 and 20 and over a unit Reynolds number range of 2 million to 7 million per foot. Two basic shapes, a hemisphere and a half-angle biconic configuration with and without nose bluntness, were tested with different surface roughness. The results are reported and discussed. (Modified author abstract).
Book Synopsis Laminar Heat-transfer and Pressure-distribution Studies on a Series of Reentry Nose Shapes at a Mach Number of 19.4 in Helium by : Richard D. Wagner
Download or read book Laminar Heat-transfer and Pressure-distribution Studies on a Series of Reentry Nose Shapes at a Mach Number of 19.4 in Helium written by Richard D. Wagner and published by . This book was released on 1961 with total page 44 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Astronautical Research 1971 by : L.G. Napolitano
Download or read book Astronautical Research 1971 written by L.G. Napolitano and published by Springer Science & Business Media. This book was released on 2012-12-06 with total page 561 pages. Available in PDF, EPUB and Kindle. Book excerpt: The International Astronautical Federation is the only professional society in the field of aerospace engineering and Sciences which brings together specialists of all countries interested in the exploration and peaceful exploitation of space. At its annual Congresses a large number of invited and/or carefully selected con tributed papers are presented which cover a wide variety of topics and are distributed over a number of sessions, each one being organized by two leading scientists who later chair the session itself. Each year the selection of specific topics to be dealt with. is dictated either by significant new progress achieved in some sectors or by new developments and trends which are liable to influence substantially the objectives toward which space research and/or application of space technology will be oriented in the immediate future. A second rigorous screening, performed with the help of the Session Chairmen and carried out according to the same criteria identifies finally the papers which are published in the Proceedings. The outcome of all this is reliable and authoritative information as to the actual status and future trends of space activities, both from the research point of view and from the point of view of u~ilization and/or application.
Book Synopsis Laminar Heat-transfer and Pressure-distribution Studies on a Series of Reentry Nose Shapes at a Mach Number of 19.4 in Helium by : RICHARD D. JR. WAGNER
Download or read book Laminar Heat-transfer and Pressure-distribution Studies on a Series of Reentry Nose Shapes at a Mach Number of 19.4 in Helium written by RICHARD D. JR. WAGNER and published by . This book was released on 1961 with total page 1 pages. Available in PDF, EPUB and Kindle. Book excerpt: An experimental investigation was conducted in the 2-in. helium tunnel at the Langley Research Center at a Mach number of 19.4 to determine the pressure distributions and heat-transfer characteristics of a family of reentry nose shapes. The pressure and heat-transfer-rate distributions on the nose shapes are compared with theoretical predictions to ascertain the limitations and validity of the theories at hypersonic speeds. The experimental results were found to be adequately predicted by existing theories. Two of the nose shapes were tested with variable-length flow-separation spikes. The results obtained by previous investigators of spike-nose bodies were found to prevail at the higher Mach number of the present investigation. (Author).
Book Synopsis Investigation of the Pressure Distributions on Reentry Nose Shapes at a Mach Number of 3.55 by : Warren A. Lawson
Download or read book Investigation of the Pressure Distributions on Reentry Nose Shapes at a Mach Number of 3.55 written by Warren A. Lawson and published by . This book was released on 1960 with total page 64 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis An Experimental Study of Space Vehicle Configurations with High Lift During Reentry by : Bryan E. Richards
Download or read book An Experimental Study of Space Vehicle Configurations with High Lift During Reentry written by Bryan E. Richards and published by . This book was released on 1976 with total page 52 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Proceedings written by and published by . This book was released on 1971 with total page 604 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis A Collection of Technical Papers by :
Download or read book A Collection of Technical Papers written by and published by . This book was released on 1977 with total page 708 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Astronautical Research by : International Astronautical Federation
Download or read book Astronautical Research written by International Astronautical Federation and published by . This book was released on 1973 with total page 602 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Pressure and Heat Transfer Measurements for Hypersonic Flows Over Expansion Corners and Ahead of Ramps: Mach 5 and 8 data for expansion corner flows by : Louis G. Kaufman
Download or read book Pressure and Heat Transfer Measurements for Hypersonic Flows Over Expansion Corners and Ahead of Ramps: Mach 5 and 8 data for expansion corner flows written by Louis G. Kaufman and published by . This book was released on 1963 with total page 96 pages. Available in PDF, EPUB and Kindle. Book excerpt: "Pressure and heat transfer data were obtained for hypersonic flows over 40-degree expansion corners and ahead of ramps. Full and partial span ramps, having wedge angles up to 90 degrees, were tested at two locations on a sharp leading edge flat plate, with and without end plates. Pressure data were obtained for [M sub infinity =] 5 for model length Reynolds numbers between 1.1 and 6.6 million. Both pressure and heat transfer data were obtained for [M sub infinity =] 8 for Reynolds numbers between 1.1 and 3.3 million." -- page iii, pt.4.
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 1979 with total page 750 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.
Book Synopsis International Aerospace Abstracts by :
Download or read book International Aerospace Abstracts written by and published by . This book was released on 1971 with total page 628 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Longshot Free Piston Hypersonic Tunnel by : Bryan E. Richards
Download or read book Longshot Free Piston Hypersonic Tunnel written by Bryan E. Richards and published by . This book was released on 1968 with total page 34 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Local Heat Transfer to Blunt Noses at High Supersonic Speeds by : William E. Stoney
Download or read book Local Heat Transfer to Blunt Noses at High Supersonic Speeds written by William E. Stoney and published by . This book was released on 1957 with total page 16 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Government Reports Announcements by :
Download or read book Government Reports Announcements written by and published by . This book was released on 1972 with total page 1404 pages. Available in PDF, EPUB and Kindle. Book excerpt:
