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Book Aerodynamic Heating in Supersonic and Hypersonic Flows

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 A Visual Technique for Determining Qualitative Aerodynamic Heating Rates on Complex Configurations

Download or read book A Visual Technique for Determining Qualitative Aerodynamic Heating Rates on Complex Configurations written by P. Calvin Stainback and published by . This book was released on 1960 with total page 34 pages. Available in PDF, EPUB and Kindle. Book excerpt: An experimental investigation was conducted at a test-section Mach number of 4.95 and a stagnation temperature of 400 F to evaluate a visual technique for obtaining qualitative aerodynamic heat-transfer data on complex configurations.This technique utilized a temperature-sensetive paint indicated that this technique was satisfactory for determining qualitative heat-transfer rates on various bodies, some of which exhibited complex flow patterns. The results obtained have been found useful to guide the instrumentation of quantitative heat-transfer models, to supplement quantitative heat-transfer measurements, and to make preliminary heat-transfer studies for new configurations.

Book Investigation of Numerical Techniques for Predicting Aerodynamic Heating to Flight Vehicles

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 The Prediction of Aerodynamic Heating of Fins on Re entry Vehicles

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 Aerodynamic Heating and Boundary layer Transition on a 1 10 power Nose Shape in Free Flight at Mach Numbers Up to 6 7 and Free stream Reynolds Numbers Up to 16 X 10 6

Download or read book Aerodynamic Heating and Boundary layer Transition on a 1 10 power Nose Shape in Free Flight at Mach Numbers Up to 6 7 and Free stream Reynolds Numbers Up to 16 X 10 6 written by Benjamine J. Garland and published by . This book was released on 1962 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Fundamentals of Aerodynamic Heating

Download or read book Fundamentals of Aerodynamic Heating written by Robert Wesley Truitt and published by . This book was released on 1960 with total page 548 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book The Effects of Aerodynamic Heating and Heat Transfer on the Surface Temperature of a Body of Revolution in Steady Supersonic Flight

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 Measurement of Aerodynamic Heat Transfer to a Deflected Trailing edge Flap on a Delta Fin in Free Flight at Mach Numbers from 1 5 to 2 6

Download or read book Measurement of Aerodynamic Heat Transfer to a Deflected Trailing edge Flap on a Delta Fin in Free Flight at Mach Numbers from 1 5 to 2 6 written by Leo T. Chauvin and published by . This book was released on 1960 with total page 22 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Measurements of Aerodynamic Heat Transfer and Boundary layer Transition on a 150 Cone in Free Flight at Supersonic Mach Numbers Up to 5 2

Download or read book Measurements of Aerodynamic Heat Transfer and Boundary layer Transition on a 150 Cone in Free Flight at Supersonic Mach Numbers Up to 5 2 written by Charles B. Rumsey and published by . This book was released on 1961 with total page 48 pages. Available in PDF, EPUB and Kindle. Book excerpt: Abstract: