On the Space Shuttle Wing Thermal-structural Analysis

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ISBN 13 :
Total Pages : 338 pages
Book Rating : 4.:/5 (12 download)

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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:

On the Space Shuttle Wing Thermal-structure Analysis

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ISBN 13 :
Total Pages : 169 pages
Book Rating : 4.:/5 (114 download)

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Book Synopsis On the Space Shuttle Wing Thermal-structure Analysis by : Kumar Krishna Tamma

Download or read book On the Space Shuttle Wing Thermal-structure Analysis written by Kumar Krishna Tamma and published by . This book was released on 1983 with total page 169 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Thermal Stress Analysis of Space Shuttle Orbiter Subjected to Reentry Aerodynamic Heating

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ISBN 13 :
Total Pages : 44 pages
Book Rating : 4.:/5 (317 download)

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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:

Thermal Stress Analysis of Space Shuttle Orbiter Wing Skin Panel and Thermal Protection System

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ISBN 13 :
Total Pages : 30 pages
Book Rating : 4.:/5 (317 download)

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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:

Thermal Response of Space Shuttle Wing During Reentry Heating

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ISBN 13 :
Total Pages : 22 pages
Book Rating : 4.:/5 (317 download)

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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:

Effect of Element Size on the Solution Accuracies of Finite-element Heat Transfer and Thermal Stress Analyses of Space Shuttle Orbiter

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ISBN 13 :
Total Pages : 56 pages
Book Rating : 4.:/5 (317 download)

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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:

Effect of Internal Convection and Internal Radiation on the Structural Temperatures of Space Shuttle Orbiter

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Publisher : Createspace Independent Publishing Platform
ISBN 13 : 9781722190507
Total Pages : 34 pages
Book Rating : 4.1/5 (95 download)

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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...

Finite-element Reentry Heat-transfer Analysis of Space Shuttle Orbiter

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Publisher :
ISBN 13 :
Total Pages : 64 pages
Book Rating : 4.:/5 (317 download)

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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:

Finite-element Reentry Heat-transfer Analysis of Space Shuttle Orbiter

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Publisher :
ISBN 13 :
Total Pages : 64 pages
Book Rating : 4.:/5 (31 download)

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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:

Space Shuttle Orbiter Thermal Protection System Design and Flight Experience

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ISBN 13 :
Total Pages : 24 pages
Book Rating : 4.:/5 (317 download)

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Book Synopsis Space Shuttle Orbiter Thermal Protection System Design and Flight Experience by : Donald M. Curry

Download or read book Space Shuttle Orbiter Thermal Protection System Design and Flight Experience written by Donald M. Curry and published by . This book was released on 1993 with total page 24 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Thermal and Structural Analysis of a Hollow Core Space Shuttle Main Engine (SSME) Turbine Blade

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Publisher :
ISBN 13 :
Total Pages : 24 pages
Book Rating : 4.:/5 (317 download)

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Book Synopsis Thermal and Structural Analysis of a Hollow Core Space Shuttle Main Engine (SSME) Turbine Blade by :

Download or read book Thermal and Structural Analysis of a Hollow Core Space Shuttle Main Engine (SSME) Turbine Blade written by and published by . This book was released on 1995 with total page 24 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Optimum Element Density Studies for Finite-element Thermal Analysis of Hypersonic Aircraft Structures

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Publisher :
ISBN 13 :
Total Pages : 44 pages
Book Rating : 4.:/5 (317 download)

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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:

Scientific and Technical Aerospace Reports

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Publisher :
ISBN 13 :
Total Pages : 1134 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis Scientific and Technical Aerospace Reports by :

Download or read book Scientific and Technical Aerospace Reports written by and published by . This book was released on 1989 with total page 1134 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Effects of Forced and Free Convections on Structural Temperatures of Space Shuttle Orbiter During Reentry Flight

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Publisher :
ISBN 13 :
Total Pages : 22 pages
Book Rating : 4.:/5 (317 download)

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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:

Computational Aspects of Heat Transfer in Structures

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ISBN 13 :
Total Pages : 596 pages
Book Rating : 4.E/5 ( download)

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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:

Optimum Element Density Studies for Finite-element Thermal Analysis of Hypersonic Aircraft Structures

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Publisher :
ISBN 13 :
Total Pages : 44 pages
Book Rating : 4.:/5 (31 download)

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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:

Thermal-structural Combined Loads Design Criteria Study

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ISBN 13 :
Total Pages : 292 pages
Book Rating : 4.:/5 (317 download)

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Book Synopsis Thermal-structural Combined Loads Design Criteria Study by : V. Deriugin

Download or read book Thermal-structural Combined Loads Design Criteria Study written by V. Deriugin and published by . This book was released on 1972 with total page 292 pages. Available in PDF, EPUB and Kindle. Book excerpt: A study was conducted to determine methodology for combining thermal structural loads and assessing the effects of the combined loads on the design of a thermal protection system and a hot structure of a high cross range delta wing space shuttle orbiter vehicle. The study presents guidelines for establishing a basis for predicting thermal and pressure environments and for determining limit and ultimate design loads on the vehicle during reentry. Limit trajectories were determined by using dispersions on a representative nominal mission and system parameters expected during the life of the vehicle. Nine chosen locations on the vehicle surface having TPS or hot structures were examined, and weight sensitivity analyses were performed for each location.