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Finite Element Reentry Heat Transfer Analysis Of Space Shuttle Orbiter
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Book Synopsis Finite-element Reentry Heat-transfer Analysis of Space Shuttle Orbiter by : Robert L. Ko
Download or read book Finite-element Reentry Heat-transfer Analysis of Space Shuttle Orbiter written by Robert L. Ko and published by . This book was released on 1986 with total page 57 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Finite-element Reentry Heat-transfer Analysis of Space Shuttle Orbiter by : William L. Ko
Download or read book Finite-element Reentry Heat-transfer Analysis of Space Shuttle Orbiter written by William L. Ko and published by . This book was released on 1986 with total page 64 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Thermal Stress Analysis of Space Shuttle Orbiter Subjected to Reentry Aerodynamic Heating by :
Download or read book Thermal Stress Analysis of Space Shuttle Orbiter Subjected to Reentry Aerodynamic Heating written by and published by . This book was released on 1987 with total page 44 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author :National Aeronautics and Space Administration (NASA) Publisher :Createspace Independent Publishing Platform ISBN 13 :9781722190507 Total Pages :34 pages Book Rating :4.1/5 (95 download)
Book Synopsis Effect of Internal Convection and Internal Radiation on the Structural Temperatures of Space Shuttle Orbiter by : National Aeronautics and Space Administration (NASA)
Download or read book Effect of Internal Convection and Internal Radiation on the Structural Temperatures of Space Shuttle Orbiter written by National Aeronautics and Space Administration (NASA) and published by Createspace Independent Publishing Platform. This book was released on 2018-07-03 with total page 34 pages. Available in PDF, EPUB and Kindle. Book excerpt: Structural performance and resizing of the finite-element thermal analysis computer program was used in the reentry heat transfer analysis of the space shuttle orbiter. One midfuselage cross section and one midspan wing segment were selected to study the effects of internal convection and internal radiation on the structural temperatures. The effect of internal convection was found to be more prominent than that of internal radiation in the orbiter thermal analysis. Without these two effects, the calculated structural temperatures at certain stations could be as much as 45 to 90 percent higher than the measured values. By considering internal convection as free convection, the correlation between the predicted and measured structural temperatures could be improved greatly. Ko, William L. and Quinn, Robert D. and Gong, Leslie Ames Research Center RTOP 532-09-01...
Book Synopsis Thermal Response of Space Shuttle Wing During Reentry Heating by :
Download or read book Thermal Response of Space Shuttle Wing During Reentry Heating written by and published by . This book was released on 1984 with total page 22 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Effect of Element Size on the Solution Accuracies of Finite-element Heat Transfer and Thermal Stress Analyses of Space Shuttle Orbiter by :
Download or read book Effect of Element Size on the Solution Accuracies of Finite-element Heat Transfer and Thermal Stress Analyses of Space Shuttle Orbiter written by and published by . This book was released on 1987 with total page 56 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Effects of Forced and Free Convections on Structural Temperatures of Space Shuttle Orbiter During Reentry Flight by : William L. Ko
Download or read book Effects of Forced and Free Convections on Structural Temperatures of Space Shuttle Orbiter During Reentry Flight written by William L. Ko and published by . This book was released on 1986 with total page 22 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Optimum Element Density Studies for Finite-element Thermal Analysis of Hypersonic Aircraft Structures by : William L. Ko
Download or read book Optimum Element Density Studies for Finite-element Thermal Analysis of Hypersonic Aircraft Structures written by William L. Ko and published by . This book was released on 1990 with total page 44 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Computational Aspects of Heat Transfer in Structures by :
Download or read book Computational Aspects of Heat Transfer in Structures written by and published by . This book was released on 1982 with total page 596 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Thermal Stress Analysis of Space Shuttle Orbiter Wing Skin Panel and Thermal Protection System by :
Download or read book Thermal Stress Analysis of Space Shuttle Orbiter Wing Skin Panel and Thermal Protection System written by and published by . This book was released on 1987 with total page 30 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book NASA Technical Memorandum written by and published by . This book was released on 1990 with total page 560 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis On the Space Shuttle Wing Thermal-structural Analysis by : Kumar Krishna Tamma
Download or read book On the Space Shuttle Wing Thermal-structural Analysis written by Kumar Krishna Tamma and published by . This book was released on 1983 with total page 338 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Computational Aspects of Heat Transfer in Structures by : Howard M. Adelman
Download or read book Computational Aspects of Heat Transfer in Structures written by Howard M. Adelman and published by . This book was released on 1982 with total page 588 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Heat-transfer and Flow-field Tests of the McDonnell Douglas-Martin Marietta Space Shuttle Configurations by : Richard K. Matthews
Download or read book Heat-transfer and Flow-field Tests of the McDonnell Douglas-Martin Marietta Space Shuttle Configurations written by Richard K. Matthews and published by . This book was released on 1973 with total page 112 pages. Available in PDF, EPUB and Kindle. Book excerpt: Aerothermodynamic tests of Phase B space shuttle configurations proposed by McDonnell Douglas--Martin Marietta were conducted at Mach numbers 8 and 10.5. 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 analysis which includes leeside heating, windward shock angles and flow fields, windward surface heating, and boundary-layer transition.
Book Synopsis Experimental Assessment of a Computer Program Used in Space Shuttle Orbiter Entry Heating Analysis by :
Download or read book Experimental Assessment of a Computer Program Used in Space Shuttle Orbiter Entry Heating Analysis written by and published by . This book was released on 1983 with total page 28 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Space Shuttle Orbiter Trimmed Center-of-gravity Extension Study. Volume 3: Impact of Retrofits for Center-of-gravity Extension on Orbiter Thermal-protection System by :
Download or read book Space Shuttle Orbiter Trimmed Center-of-gravity Extension Study. Volume 3: Impact of Retrofits for Center-of-gravity Extension on Orbiter Thermal-protection System written by and published by . This book was released on 1979 with total page 44 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book NASA Technical Paper written by and published by . This book was released on 1987 with total page 532 pages. Available in PDF, EPUB and Kindle. Book excerpt: