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

Thermal Stress Analysis of Space Shuttle Orbiter Wing Skin Panel and Thermal Protection System PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 30

Book Description


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

Thermal Stress Analysis of Space Shuttle Orbiter Wing Skin Panel and Thermal Protection System PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 30

Book Description


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

Thermal Stress Analysis of Space Shuttle Orbiter Subjected to Reentry Aerodynamic Heating PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 44

Book Description


Scientific and Technical Aerospace Reports

Scientific and Technical Aerospace Reports PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 892

Book Description


NASA Tech Briefs

NASA Tech Briefs PDF Author:
Publisher:
ISBN:
Category : Technology
Languages : en
Pages : 1282

Book Description


Thermostructural Analysis of Unconventional Wing Structures of a Hyper-X Hypersonic Flight Research Vehicle for the Mach 7 Mission

Thermostructural Analysis of Unconventional Wing Structures of a Hyper-X Hypersonic Flight Research Vehicle for the Mach 7 Mission PDF Author: William L. Ko
Publisher:
ISBN:
Category : Aerodynamic heating
Languages : en
Pages : 46

Book Description
Heat transfer, thermal stresses, and thermal buckling analyses were performed on the unconventional wing structures of a Hyper-X hypersonic flight research vehicle (designated as X-43) subject to nominal Mach 7 aerodynamic heating. A wing midspan cross was selected for the the heat transfer and thermal stress analyses. Thermal buckling analysis was performed on three regions of the wing skin (lower or upper); 1) a fore wing panel, 2) an aft wing panel, and 3) a unit panel at the middle of the aft wing panel. A fourth thermal buckling analysis was performed on a midspan wing segment. The unit panel region is identified as the potential thermal buckling initiation zone. Therefore, thermal buckling analysis of the Hyper-X wing panels could be reduced to the thermal buckling analysis of that unit panel. "Buckling temperature magnification factors" were established. Structural temperature-time histories are presented. The results show that the concerns of shear failure at wing and spar welded sites.

Monthly Catalog of United States Government Publications

Monthly Catalog of United States Government Publications PDF Author:
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1248

Book Description


Monthly Catalogue, United States Public Documents

Monthly Catalogue, United States Public Documents PDF Author:
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1508

Book Description


Monthly Catalog of United States Government Publications

Monthly Catalog of United States Government Publications PDF Author:
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 826

Book Description


AIAA 84-0101 - AIAA 84-0150

AIAA 84-0101 - AIAA 84-0150 PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 558

Book Description


Government Reports Annual Index

Government Reports Annual Index PDF Author:
Publisher:
ISBN:
Category : Research
Languages : en
Pages : 1030

Book Description
Sections 1-2. Keyword Index.--Section 3. Personal author index.--Section 4. Corporate author index.-- Section 5. Contract/grant number index, NTIS order/report number index 1-E.--Section 6. NTIS order/report number index F-Z.