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An Axisymmetric Analog Two Layer Convective Heating Procedure With Application To The Evaluation Of Space Shuttle Orbiter Wing Leading Edge And Windward Surface Heating
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Author :National Aeronautics and Space Administration (NASA) Publisher :Createspace Independent Publishing Platform ISBN 13 :9781722935573 Total Pages :148 pages Book Rating :4.9/5 (355 download)
Book Synopsis An Axisymmetric Analog Two-Layer Convective Heating Procedure with Application to the Evaluation of Space Shuttle Orbiter Wing Leading Edge and Windward Surface Heating by : National Aeronautics and Space Administration (NASA)
Download or read book An Axisymmetric Analog Two-Layer Convective Heating Procedure with Application to the Evaluation of Space Shuttle Orbiter Wing Leading Edge and Windward Surface Heating written by National Aeronautics and Space Administration (NASA) and published by Createspace Independent Publishing Platform. This book was released on 2018-07-17 with total page 148 pages. Available in PDF, EPUB and Kindle. Book excerpt: A numerical procedure for predicting the convective heating rate of hypersonic reentry vehicles is described. The procedure, which is based on the axisymmetric analog, consists of obtaining the three-dimensional inviscid flowfield solution; then the surface streamlines and metrics are calculated using the inviscid velocity components on the surface; finally, an axisymmetric boundary layer code or approximate convective heating equations are used to evaluate heating rates. This approach yields heating predictions to general three-dimensional body shapes. The procedure has been applied to the prediction of the wing leading edge heating to the Space Shuttle Orbiter. The numerical results are compared with the results of heat transfer testing (OH66) of an 0.025 scale model of the Space Shuttle Orbiter configuration in the Calspan Hypersonic Shock Tunnel (HST) at Mach 10 and angles of attack of 30 and 40 degrees. Comparisons with STS-5 flight data at Mach 9.15 and angle of attack of 37.4 degrees and STS-2 flight data at Mach 12.86 and angle of attack of 39.7 degrees are also given. Wang, K. C. Unspecified Center AERODYNAMIC HEATING; COMPUTATIONAL FLUID DYNAMICS; CONVECTIVE HEAT TRANSFER; HYPERSONIC HEAT TRANSFER; INVISCID FLOW; SPACE SHUTTLE ORBITERS; ANGLE OF ATTACK; BOUNDARY LAYERS; HYPERSONIC SPEED; LEADING EDGES; THREE DIMENSIONAL BODIES...
Book Synopsis An Axisymmetric Analog Two-layer Convective Heating Procedure with Application to the Evaluation of Space Shuttle Orbiter Wing Leading Edge and Windward Surface Heating by :
Download or read book An Axisymmetric Analog Two-layer Convective Heating Procedure with Application to the Evaluation of Space Shuttle Orbiter Wing Leading Edge and Windward Surface Heating written by and published by . This book was released on 1994 with total page 154 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Scientific and Technical Aerospace Reports by :
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Book Synopsis A Method for Calculating Transient Surface Temperatures and Surface Heating Rates for High-speed Aircraft by : Robert D. Quinn
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Book Synopsis Approximate Method of Predicting Heating on the Windward Side of Space Shuttle Orbiter and Comparisons with Flight Data by : H. H. Hamilton
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Book Synopsis Calculation of Laminar Heating Rates on Three-dimensional Configurations Using the Axisymmetric Analogue by : H. H. Hamilton (II)
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Book Synopsis Heating Measurements on Space Shuttle Orbiter Models with Differentially Deflected Elevons by :
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Book Synopsis Calculation of Laminar Heating Rates on Three-dimensional Configurations Using the Axisymmetric Analogue by : H. Harris Hamilton
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Book Synopsis Experimental Aerodynamic Heating to Simulated Space Shuttle Tiles in Laminar and Turbulent Boundary Layers with Variable Flow Angles at a Nominal Mach Number of 7 by : Don E. Avery
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Book Synopsis Aerodynamic Heating of a Space Shuttle Delta-wing Orbiter by :
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Book Synopsis Aeroheating Predictions for X-34 Using an Inviscid-Boundary Layer Method by : Christropher J. Riley
Download or read book Aeroheating Predictions for X-34 Using an Inviscid-Boundary Layer Method written by Christropher J. Riley and published by . This book was released on 1998 with total page 34 pages. Available in PDF, EPUB and Kindle. Book excerpt:
