Heat-transfer and Flow-field Tests of the North American Rockwell/ General Dynamics Convair Space Shuttle Configurations

Heat-transfer and Flow-field Tests of the North American Rockwell/ General Dynamics Convair Space Shuttle Configurations
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Publisher :
Total Pages : 100
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ISBN-10 : UOM:39015104952471
ISBN-13 :
Rating : 4/5 ( Downloads)

Book Synopsis Heat-transfer and Flow-field Tests of the North American Rockwell/ General Dynamics Convair Space Shuttle Configurations by : W. R. Martindale

Download or read book Heat-transfer and Flow-field Tests of the North American Rockwell/ General Dynamics Convair Space Shuttle Configurations written by W. R. Martindale and published by . This book was released on 1973 with total page 100 pages. Available in PDF, EPUB and Kindle. Book excerpt: Aerothermodynamic tests of Phase B space shuttle configurations proposed by North American Rockwell/General Dynamics Convair were conducted at Mach number 8. Test conditions provided both Mach number and Reynolds number simulation for typical ascent and reentry trajectories. This report provides a comprehensive analysis of the major test results and also presents data comparisons with theoretical calculations. Specific areas covered are: ascent heating and shock interference, booster reentry heating and flow fields, and orbiter reentry including leeside heating, windward shock angles and flow fields, windward surface heating, and boundary-layer transition.


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