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Comparison Of Flight Measured And Calculated Temperatures On The Space Shuttle Orbiter
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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:
Book Synopsis A Method for Calculating Transient Surface Temperatures and Surface Heating Rates for High-speed Aircraft by : Robert D. Quinn
Download or read book A Method for Calculating Transient Surface Temperatures and Surface Heating Rates for High-speed Aircraft written by Robert D. Quinn and published by . This book was released on 2000 with total page 38 pages. Available in PDF, EPUB and Kindle. Book excerpt: This report describes a method that can calculate transient aerodynamic heating and transient surface temperatures at supersonic and hypersonic speeds. This method can rapidly calculate temperature and heating rate time-histories for complete flight trajectories. Semi-empirical theories are used to calculate laminar and turbulent heat transfer coefficients and a procedure for estimating boundary-layer transition is included. Results from this method are compared with flight data from the X-15 research vehicle, YF-12 airplane, and the Space Shuttle Orbiter. These comparisons show that the calculated values are in good agreement with the measured flight data.
Author :National Aeronautics and Space Administration (NASA) Publisher :Createspace Independent Publishing Platform ISBN 13 :9781720361053 Total Pages :36 pages Book Rating :4.3/5 (61 download)
Book Synopsis A Method for Calculating Transient Surface Temperatures and Surface Heating Rates for High-Speed Aircraft by : National Aeronautics and Space Administration (NASA)
Download or read book A Method for Calculating Transient Surface Temperatures and Surface Heating Rates for High-Speed Aircraft written by National Aeronautics and Space Administration (NASA) and published by Createspace Independent Publishing Platform. This book was released on 2018-05-30 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt: This report describes a method that can calculate transient aerodynamic heating and transient surface temperatures at supersonic and hypersonic speeds. This method can rapidly calculate temperature and heating rate time-histories for complete flight trajectories. Semi-empirical theories are used to calculate laminar and turbulent heat transfer coefficients and a procedure for estimating boundary-layer transition is included. Results from this method are compared with flight data from the X-15 research vehicle, YF-12 airplane, and the Space Shuttle Orbiter. These comparisons show that the calculated values are in good agreement with the measured flight data.Quinn, Robert D. and Gong, LeslieArmstrong Flight Research CenterSURFACE TEMPERATURE; COMPUTATION; PROCEDURES; TRANSIENT HEATING; ESTIMATING; SUPERSONIC SPEED; SPACE SHUTTLE ORBITERS; YF-12 AIRCRAFT; BOUNDARY LAYER TRANSITION; HEAT TRANSFER COEFFICIENTS; LAMINAR HEAT TRANSFER; RESEARCH VEHICLES
Book Synopsis Comparison of Space Shuttle Orbiter Wing Leading Edge Heating Rate Calculations with Experimental and Flight Data by : K. C. Wang
Download or read book Comparison of Space Shuttle Orbiter Wing Leading Edge Heating Rate Calculations with Experimental and Flight Data written by K. C. Wang and published by . This book was released on 1994 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
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 1994 with total page 956 pages. Available in PDF, EPUB and Kindle. Book excerpt:
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 Experimental Assessment of a Computer Program Used in Space Shuttle Orbiter Entry Heating Analyses by : William L. Wells
Download or read book Experimental Assessment of a Computer Program Used in Space Shuttle Orbiter Entry Heating Analyses written by William L. Wells and published by . This book was released on 1983 with total page 28 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:
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 A Comparison of Laboratory Measured Temperatures with Predictions for a Spar/skin Type Aircraft Structure by :
Download or read book A Comparison of Laboratory Measured Temperatures with Predictions for a Spar/skin Type Aircraft Structure written by and published by . This book was released on 1981 with total page 30 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 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 Flight Measurements of Airplane Structural Temperatures at Supersonic Speeds by : Richard D. Banner
Download or read book Flight Measurements of Airplane Structural Temperatures at Supersonic Speeds written by Richard D. Banner and published by . This book was released on 1957 with total page 20 pages. Available in PDF, EPUB and Kindle. Book excerpt: Summary: Skin and structural temperatures have been obtained on the X-1B and X-1E research airplanes under transient aerodynamic heating conditions at speeds up to Mach numbers near 2.0. Extensive temperature measurements were obtained throughout the X-1B airplane, and temperature distributions are shown on the nose cone, the wing, and the vertical tail. Temperatures for the X-1E wing leading edge and internal wing structure were compared with similar data for the X-1B. No critical skin and structural temperatures were obtained on the two airplanes over the range of these tests. Simplified calculations of the skin temperatures in the laminar-flow regions of the nose cone and the leading edges agreed favorably with the general trends in the measured data. The flat-plate skin-temperature calculations in the turbulent-flow regions agreed favorably with the measured data on the nose cone and at the midsemispan station of the wing but overestimated the vertical-tail skin temperatures and also the upper wing skin temperature near the wing tip. The relatively low values of the upper skin temperatures that were measured at the wing tip were believed to be caused by separated-flow effects in this region.
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 Numerical Methods in Thermal Problems by : Roland Wynne Lewis
Download or read book Numerical Methods in Thermal Problems written by Roland Wynne Lewis and published by Swansea : Pineridge Press. This book was released on 1987 with total page 1178 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Numerical Methods in Thermal Problems by :
Download or read book Numerical Methods in Thermal Problems written by and published by . This book was released on 1987 with total page 1014 pages. Available in PDF, EPUB and Kindle. Book excerpt: