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Aerodynamic Heating Of Conical Entry Vehicles At Speeds In Excess Of Earth Parabolic Speed With List Of References
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Book Synopsis Aerodynamic Heating of Conical Entry Vehicles at Speeds in Excess of Earth Parabolic Speed by : H. J. Allen
Download or read book Aerodynamic Heating of Conical Entry Vehicles at Speeds in Excess of Earth Parabolic Speed written by H. J. Allen and published by . This book was released on 1963 with total page 112 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Aerodynamic Heating of Conical Entry Vehicles at Speeds in Excess of Earth Parabolic Speed [with List of References] by :
Download or read book Aerodynamic Heating of Conical Entry Vehicles at Speeds in Excess of Earth Parabolic Speed [with List of References] written by and published by . This book was released on 1963 with total page 97 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Aerodynamic Heating of Conical Entry Vehicles at Speeds in Excess of Earth Parabolic Speed by :
Download or read book Aerodynamic Heating of Conical Entry Vehicles at Speeds in Excess of Earth Parabolic Speed written by and published by . This book was released on 1965 with total page 1 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Monthly Catalogue, United States Public Documents by :
Download or read book Monthly Catalogue, United States Public Documents written by and published by . This book was released on 1965 with total page 1732 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Monthly Catalog of United States Government Publications by :
Download or read book Monthly Catalog of United States Government Publications written by and published by . This book was released on 1965 with total page 1550 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis The Effects of Aerodynamic Heating and Heat Transfer on the Surface Temperature of a Body of Revolution in Steady Supersonic Flight by : Richard Scherrer
Download or read book The Effects of Aerodynamic Heating and Heat Transfer on the Surface Temperature of a Body of Revolution in Steady Supersonic Flight written by Richard Scherrer and published by . This book was released on 1947 with total page 542 pages. Available in PDF, EPUB and Kindle. Book excerpt: An approximate method for determining the convective cooling requirement in the laminar-boundary-layer region of a body of revolution in high-speed flight was developed and applied to an example body. The cooling requirement for the example body was determined as a function of Mach number, altitude, size, and a surface-temperature parameter. The maximum value of Mach number considered was 3.0 and the altitudes considered were those within the lower constant-temperature region of the atmosphere (40,000 to 120,000 ft). The extent of the laminar boundary layer was determined approximately at each condition as a function of the variables considered.
Book Synopsis Investigation of Numerical Techniques for Predicting Aerodynamic Heating to Flight Vehicles by : Arthur B. Lewis (Jr.)
Download or read book Investigation of Numerical Techniques for Predicting Aerodynamic Heating to Flight Vehicles written by Arthur B. Lewis (Jr.) and published by . This book was released on 1979 with total page 122 pages. Available in PDF, EPUB and Kindle. Book excerpt: The development of complex lifting configurations and high speed maneuvering vehicles has emphasized the need for numerical techniques to predict aerodynamic heating rates as a function of the vehicle trajectory. These numerical programs are not expected to eliminate the requirements for wind tunnel and flight testing, but will be an aid to more efficient use of experimentation time and improve confidence that all potential problem areas on the vehicle have been examined. Three programs, the Hypersonic Arbitrary Body Program, the MINIVER Program, and a third program were examined to determine their usefulness for vehicles with non-circular cross sections and large flat areas as exemplified by lifting reentry vehicles. The MINIVER code was found to be unsuitable for this; the Hypersonic Arbitrary Body Program was applicable to these shapes, but because of program limitations was used for only limited calculations. The last program also had limitations in the areas of geometry description and surface pressure calculations. Efforts were made to remove these limitations and several shapes were investigated. The ultimate goal of this effort was to extend the capabilities of one or more of the heating codes; while no effort was made to improve MINIVER or the Hypersonic Arbitrary Body Program, significant improvements were made in the last program and inviscid flow field program.
Book Synopsis Convective Heat-transfer Rates on Large-scale Conical Bodies at Hypersonic Speeds by : David Alexander Stewart
Download or read book Convective Heat-transfer Rates on Large-scale Conical Bodies at Hypersonic Speeds written by David Alexander Stewart and published by . This book was released on 1969 with total page 28 pages. Available in PDF, EPUB and Kindle. Book excerpt: Heat-transfer rates were measured on large-angle conical bodies with large half-angles between 50 degrees and 90 degrees, at angles of attack from 0 degrees. The results at 0 degree angle of attack were predicted with Lees' similarity theory, using calculated flow properties at the boundary-layer edge. The calculated flow properties were obtained from Newtonian theory for the 50 degree cone and from a one- or two-strip solution using the method of integral relations for other cones. At 0 degree angle of attack, an increase in cone angle resulted in a decrease in the heating rate over much of the body. However, high heating rates occurred at the shoulder of the both the half-angle = 80 degree and half-angle =90 degree shapes because of local pressure gradients. On the windward side of the cones, the heating rate increased with angle of attack.
Book Synopsis The Prediction of Aerodynamic Heating of Fins on Re-entry Vehicles by : E. C. Lemmon
Download or read book The Prediction of Aerodynamic Heating of Fins on Re-entry Vehicles written by E. C. Lemmon and published by . This book was released on 1971 with total page 64 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Measurements of Aerodynamic Heat Transfer in Turbulent Separated Regions at a Mach Number of 1.8 by : Benjamine J. Garland
Download or read book Measurements of Aerodynamic Heat Transfer in Turbulent Separated Regions at a Mach Number of 1.8 written by Benjamine J. Garland and published by . This book was released on 1958 with total page 20 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book National Union Catalog written by and published by . This book was released on 1968 with total page 632 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Aerodynamic Heating and the Deflection of Drops by an Obstacle in an Air Stream in Relation to Aircraft Icing by : Arthur Kantrowitz
Download or read book Aerodynamic Heating and the Deflection of Drops by an Obstacle in an Air Stream in Relation to Aircraft Icing written by Arthur Kantrowitz and published by . This book was released on 1940 with total page 22 pages. Available in PDF, EPUB and Kindle. Book excerpt: Numerical calculations of the paths of water drops in an air stream around a circular cylinder are given. From these calculations, information is obtained on the percentage of the swept area cleared of drops.
Book Synopsis Free-flight Measurements of Aerodynamic Heat Transfer to Mach Number 3.9 and of Drag to Mach Number 6.9 of a Fin-stabilized Cone-cylinder Configuration by : Charles B. Rumsey
Download or read book Free-flight Measurements of Aerodynamic Heat Transfer to Mach Number 3.9 and of Drag to Mach Number 6.9 of a Fin-stabilized Cone-cylinder Configuration written by Charles B. Rumsey and published by . This book was released on 1955 with total page 26 pages. Available in PDF, EPUB and Kindle. Book excerpt: Aerodynamic-heat-transfer measurements have been made at a station on the 10 degree total angle conical nose of a rocket-propelled model at flight Mach numbers of 1.4 to 3.9. The corresponding values of local Reynolds number varied from 18,000,000 to 46,000,000 and the ratio of skin temperature to local static temperature varied from 1.2 to 2.4. The experimental data, reduced to Stanton number, were in fair agreement with values predicted by Van Driest's theory for heat transfer on a cone with turbulent flow from the nose tip.
Book Synopsis The National Union Catalogs, 1963- by :
Download or read book The National Union Catalogs, 1963- written by and published by . This book was released on 1964 with total page 630 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Proceedings of a Conference on Aerodynamically Heated Structures Held at Cambridge, Massachusetts, July 25, 1961 by :
Download or read book Proceedings of a Conference on Aerodynamically Heated Structures Held at Cambridge, Massachusetts, July 25, 1961 written by and published by . This book was released on 1962 with total page 368 pages. Available in PDF, EPUB and Kindle. Book excerpt: This volume brings together for the first time papers by recognized authorities on the structural and materials requirements of space vehicles exposed to aerodynamic heating, particularly during re-entry. The current status of insulating problems, especially in lift-flight vehicles, is discussed in detail, as are proposed thermal protection systems for future aerospace vehicles. Of particular importance are the reports on new developments of high-temperature thermal protection systems, thermal protection of cryogenic propellants, and structural cooling systems. (Author).
Author :Earl Arthur Thornton Publisher :AIAA (American Institute of Aeronautics & Astronautics) ISBN 13 : Total Pages :576 pages Book Rating :4.3/5 (91 download)
Book Synopsis Thermal Structures and Materials for High-speed Flight by : Earl Arthur Thornton
Download or read book Thermal Structures and Materials for High-speed Flight written by Earl Arthur Thornton and published by AIAA (American Institute of Aeronautics & Astronautics). This book was released on 1992 with total page 576 pages. Available in PDF, EPUB and Kindle. Book excerpt: This text presents recent research and development in aerothermodynamics, advanced light metals and composites, thermal structures, materials performance and failure criteria, and intelligent processing of materials, as they relate to high-speed flight. Researchers and designers of aerospace vehicles for high-speed flight, as well as materials scientists, should find this text valuable.
Book Synopsis Aerodynamic Heating in the Vicinity of Corners at Hypersonic Speeds by : P. Calvin Stainback
Download or read book Aerodynamic Heating in the Vicinity of Corners at Hypersonic Speeds written by P. Calvin Stainback and published by . This book was released on 1967 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt: