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Experimental Determination Of Convective Heat Transfer Coefficients In The Separated Flow Region Of The Space Shuttle Solid Rocket Motor
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Book Synopsis Experimental Determination of Convective Heat Transfer Coefficients in the Separated Flow Region of the Space Shuttle Solid Rocket Motor by : R. Harold Whitesides
Download or read book Experimental Determination of Convective Heat Transfer Coefficients in the Separated Flow Region of the Space Shuttle Solid Rocket Motor written by R. Harold Whitesides and published by . This book was released on 1990 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis FY 1990 Scientific and Technical Reports, Articles, Papers, and Presentations by :
Download or read book FY 1990 Scientific and Technical Reports, Articles, Papers, and Presentations written by and published by . This book was released on 1990 with total page 78 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis AIAA 28th Aerospace Sciences Meeting by :
Download or read book AIAA 28th Aerospace Sciences Meeting written by and published by . This book was released on 1990 with total page 472 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Application of Various Techniques for Determining Local Heat-transfer Coefficients in a Rocket Engine from Transient Experimental Data by : Curt H. Liebert
Download or read book Application of Various Techniques for Determining Local Heat-transfer Coefficients in a Rocket Engine from Transient Experimental Data written by Curt H. Liebert and published by . This book was released on 1960 with total page 38 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis 30th AIAA/ASME/SAE/ASEE Joint Propulsion Conference by :
Download or read book 30th AIAA/ASME/SAE/ASEE Joint Propulsion Conference written by and published by . This book was released on 1994 with total page 730 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 1992 with total page 1572 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 1994 with total page 492 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Aerospace America written by and published by . This book was released on 1989 with total page 650 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Experimental Determination of the Coefficient of Convective Heat Transfer in High Temperature Fluid Flow by : A. Knapp
Download or read book Experimental Determination of the Coefficient of Convective Heat Transfer in High Temperature Fluid Flow written by A. Knapp and published by . This book was released on 1987 with total page 12 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author :American Institute of Aeronautics and Astronautics. Technical Information Service Publisher : ISBN 13 : Total Pages :180 pages Book Rating :4.3/5 (91 download)
Book Synopsis The Finding Guide to AIAA Meeting Papers by : American Institute of Aeronautics and Astronautics. Technical Information Service
Download or read book The Finding Guide to AIAA Meeting Papers written by American Institute of Aeronautics and Astronautics. Technical Information Service and published by . This book was released on 1990 with total page 180 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Variation of Convective Heat-transfer Coefficient Around a Simulated Rocket Cooling Tube Section by : Ronald G. Huff
Download or read book Variation of Convective Heat-transfer Coefficient Around a Simulated Rocket Cooling Tube Section written by Ronald G. Huff and published by . This book was released on 1969 with total page 36 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 1996 with total page 512 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Experimental Evaluation of an Oscillating Temperature Technique for Obtaining Convective Heat-transfer Coefficients by : Ronald G. Huff
Download or read book Experimental Evaluation of an Oscillating Temperature Technique for Obtaining Convective Heat-transfer Coefficients written by Ronald G. Huff and published by . This book was released on 1970 with total page 52 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Space Shuttle Aerothermodynamics Technology Conference, Held at Ames Research Center, Moffett Field, Calif., December 15-16, 1971 by :
Download or read book Space Shuttle Aerothermodynamics Technology Conference, Held at Ames Research Center, Moffett Field, Calif., December 15-16, 1971 written by and published by . This book was released on 1972 with total page 470 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Heat-transfer and Flow-field Tests of the North American Rockwell/ General Dynamics Convair Space Shuttle Configurations by : W. R. Martindale
Download or read book Heat-transfer and Flow-field Tests of the North American Rockwell/ General Dynamics Convair Space Shuttle Configurations written by W. R. Martindale and published by . This book was released on 1973 with total page 100 pages. Available in PDF, EPUB and Kindle. Book excerpt: Aerothermodynamic tests of Phase B space shuttle configurations proposed by North American Rockwell/General Dynamics Convair were conducted at Mach number 8. 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 including leeside heating, windward shock angles and flow fields, windward surface heating, and boundary-layer transition.
Author :National Aeronautics and Space Adm Nasa Publisher :Independently Published ISBN 13 :9781729326442 Total Pages :62 pages Book Rating :4.3/5 (264 download)
Book Synopsis Development of a Laser-Induced Heat Flux Technique for Measurement of Convective Heat Transfer Coefficients in a Supersonic Flowfield by : National Aeronautics and Space Adm Nasa
Download or read book Development of a Laser-Induced Heat Flux Technique for Measurement of Convective Heat Transfer Coefficients in a Supersonic Flowfield written by National Aeronautics and Space Adm Nasa and published by Independently Published. This book was released on 2018-10-27 with total page 62 pages. Available in PDF, EPUB and Kindle. Book excerpt: A technique is developed to measure the local convective heat transfer coefficient on a model surface in a supersonic flow field. The technique uses a laser to apply a discrete local heat flux at the model test surface, and an infrared camera system determines the local temperature distribution due to heating. From this temperature distribution and an analysis of the heating process, a local convective heat transfer coefficient is determined. The technique was used to measure the load surface convective heat transfer coefficient distribution on a flat plate at nominal Mach numbers of 2.5, 3.0, 3.5, and 4.0. The flat plate boundary layer initially was laminar and became transitional in the measurement region. The experimental results agreed reasonably well with theoretical predictions of convective heat transfer of flat plate laminar boundary layers. The results indicate that this non-intrusive optical measurement technique has the potential to obtain high quality surface convective heat transfer measurements in high speed flowfields. Porro, A. Robert and Keith, Theo G., Jr. and Hingst, Warren R. and Chriss, Randall M. and Seablom, Kirk D. Glenn Research Center...
Author :National Aeronautics and Space Administration (NASA) Publisher :Createspace Independent Publishing Platform ISBN 13 :9781722950767 Total Pages :102 pages Book Rating :4.9/5 (57 download)
Book Synopsis Asrm Nozzle Thermal Analysis by : National Aeronautics and Space Administration (NASA)
Download or read book Asrm Nozzle Thermal Analysis written by National Aeronautics and Space Administration (NASA) and published by Createspace Independent Publishing Platform. This book was released on 2018-07-17 with total page 102 pages. Available in PDF, EPUB and Kindle. Book excerpt: This report describes results from the nozzle thermal analysis contract which has been performed to support NASA/Marshall Space Flight Center in the development of the Advanced Solid Rocket Motor (ASRM). The emphasis of this study has been directed to four potential problem areas of the nozzle. These areas are the submerged nozzle region containing the flex seal, the nozzle entrance region, the material interface region in the nozzle exit cone, and the aft region of the exit cone. This study was limited throughout by inadequate material response models, especially for the polyisoprene flex seal and the low density carbon phenolic used in the exit cone. Thermal response and particle erosion calculations were performed for each of the potential problem areas. Results from these studies showed excessive erosion (large negative safety margins) to occur in the flex seal and nozzle entrance regions. The exit cone was found to be marginally adequate (near zero safety margins) and the material interface region was found not to be a problem. Strobel, Forrest and King, Belinda Unspecified Center ADVANCED SOLID ROCKET MOTOR (STS); EROSION; FLOW DISTRIBUTION; ROCKET NOZZLES; SAFETY FACTORS; SEALS (STOPPERS); THERMAL ANALYSIS; CARBON-PHENOLIC COMPOSITES; CONVECTIVE HEAT TRANSFER; POLYISOPRENES; TEMPERATURE EFFECTS; THERMOCHEMICAL PROPERTIES; THERMOCHEMISTRY...
