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Effects Of Forced And Free Convections On Structural Temperatures Of Space Shuttle Orbiter During Reentry Flight
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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:
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 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 1988 with total page 594 pages. Available in PDF, EPUB and Kindle. Book excerpt: Lists citations with abstracts for aerospace related reports obtained from world wide sources and announces documents that have recently been entered into the NASA Scientific and Technical Information Database.
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 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 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:
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 AIAA 87-1600 - AIAA 87-1651 (with omissions in numbering) by :
Download or read book AIAA 87-1600 - AIAA 87-1651 (with omissions in numbering) written by and published by . This book was released on 1987 with total page 660 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Hypersonics written by and published by Springer Nature. This book was released on 1989 with total page 554 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:
Book Synopsis Fifty Years of Flight Research by : David F. Fisher
Download or read book Fifty Years of Flight Research written by David F. Fisher and published by . This book was released on 1999 with total page 526 pages. Available in PDF, EPUB and Kindle. Book excerpt: A bibliography of Technical Reports from Dryden Research Center, 1946-1996. Dryden was a National Advisory Committee for Aeronautics (NACA) facility from to 1946-1958, when NACA became NASA (National Aeronautics and Space Administration). This bibliography encompasses both NACA and NASA publications. Illustrated with diagrams and photos. Black and white version.
Book Synopsis Monthly Catalog of United States Government Publications by :
Download or read book Monthly Catalog of United States Government Publications written by and published by . This book was released on 1990 with total page 882 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis International Aerospace Abstracts by :
Download or read book International Aerospace Abstracts written by and published by . This book was released on 1998 with total page 980 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Monthly Catalogue, United States Public Documents by :
Download or read book Monthly Catalogue, United States Public Documents written by and published by . This book was released on 1990 with total page 1480 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Comparison of Flight-measured and Calculated Temperatures on the Space Shuttle Orbiter by :
Download or read book Comparison of Flight-measured and Calculated Temperatures on the Space Shuttle Orbiter written by and published by . This book was released on 1987 with total page 78 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author :National Aeronautics and Space Administration (NASA) Publisher :Createspace Independent Publishing Platform ISBN 13 :9781720575788 Total Pages :44 pages Book Rating :4.5/5 (757 download)
Book Synopsis Hypothetical Reentry Thermostructural Performance of Space Shuttle Orbiter with Missing Or Eroded Thermal Protection Tiles by : National Aeronautics and Space Administration (NASA)
Download or read book Hypothetical Reentry Thermostructural Performance of Space Shuttle Orbiter with Missing Or Eroded Thermal Protection Tiles written by National Aeronautics and Space Administration (NASA) and published by Createspace Independent Publishing Platform. This book was released on 2018-05-31 with total page 44 pages. Available in PDF, EPUB and Kindle. Book excerpt: This report deals with hypothetical reentry thermostructural performance of the Space Shuttle orbiter with missing or eroded thermal protection system (TPS) tiles. The original STS-5 heating (normal transition at 1100 sec) and the modified STS-5 heating (premature transition at 800 sec) were used as reentry heat inputs. The TPS missing or eroded site is assumed to be located at the center or corner (spar-rib juncture) of the lower surface of wing midspan bay 3. For cases of missing TPS tiles, under the original STS-5 heating, the orbiter can afford to lose only one TPS tile at the center or two TPS tiles at the corner (spar-rib juncture) of the lower surface of wing midspan bay 3. Under modified STS-5 heating, the orbiter cannot afford to lose even one TPS tile at the center or at the corner of the lower surface of wing midspan bay 3. For cases of eroded TPS tiles, the aluminum skin temperature rises relatively slowly with the decreasing thickness of the eroded central or corner TPS tile until most of the TPS tile is eroded away, and then increases exponentially toward the missing tile case.Ko, William L. and Gong, Leslie and Quinn, Robert D.Armstrong Flight Research CenterSPACE SHUTTLE ORBITERS; THERMAL PROTECTION; TILES; EROSION; UNCONTROLLED REENTRY (SPACECRAFT); SPACE TRANSPORTATION SYSTEM; AEROTHERMODYNAMICS; ALUMINUM; SKIN TEMPERATURE (NON-BIOLOGICAL); AERODYNAMIC HEATING; WINGS; COLUMBIA (ORBITER); MACH NUMBER; RIBS (SUPPORTS)
Book Synopsis Roughness and Wall Temperature Effects on Boundary-Layer Transition on a 0.0175-Scale Space Shuttle Orbiter Model Tested at Mach Number 8 by : G. D. Wannenwetsch
Download or read book Roughness and Wall Temperature Effects on Boundary-Layer Transition on a 0.0175-Scale Space Shuttle Orbiter Model Tested at Mach Number 8 written by G. D. Wannenwetsch and published by . This book was released on 1977 with total page 42 pages. Available in PDF, EPUB and Kindle. Book excerpt: Heat-transfer tests were conducted on the Space Shuttle Orbiter Vehicle in the AEDC/VKF Hypersonic Wind Tunnel (B) to determine the location of boundary-layer transition for a simulated reentry phase flight profile. The model was a 0.0175-scale model with simulated randomly misaligned thermal protection system tiles etched into the windward surface. The tests were conducted at a nominal free-stream Mach number of 8, free-stream unit Reynolds numbers ranging from 0.5 million to 3.7 million per ft, and angles of attack of 30, 35, and 40 deg. Values of wall temperature to free-stream stagnation temperature ranged from 0.14 to 0.44. Representative test data and an analysis of the windward surface centerline heat-transfer data are included. Effects of wall temperature, tile roughness, and angle of attack on the location of transition are discussed.
