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Book A Study of Leeside Flow Field Heat Transfer on Shuttle Orbiter Configuration

Download or read book A Study of Leeside Flow Field Heat Transfer on Shuttle Orbiter Configuration written by and published by . This book was released on 1984 with total page 328 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Heat transfer and Flow field Tests of the North American Rockwell  General Dynamics Convair Space Shuttle Configurations

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.

Book Heat transfer and Flow field Tests of the McDonnell Douglas Martin Marietta Space Shuttle Configurations

Download or read book Heat transfer and Flow field Tests of the McDonnell Douglas Martin Marietta Space Shuttle Configurations written by Richard K. Matthews and published by . This book was released on 1973 with total page 112 pages. Available in PDF, EPUB and Kindle. Book excerpt: Aerothermodynamic tests of Phase B space shuttle configurations proposed by McDonnell Douglas--Martin Marietta were conducted at Mach numbers 8 and 10.5. 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 analysis which includes leeside heating, windward shock angles and flow fields, windward surface heating, and boundary-layer transition.

Book Scientific and Technical Aerospace Reports

Download or read book Scientific and Technical Aerospace Reports written by and published by . This book was released on 1984 with total page 1278 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Lee surface Heating and Flow Phenomena on Space Shuttle Orbiters at Large Angles of Attack and Hypersonic Speeds

Download or read book Lee surface Heating and Flow Phenomena on Space Shuttle Orbiters at Large Angles of Attack and Hypersonic Speeds written by Jerry N. Hefner and published by . This book was released on 1972 with total page 52 pages. Available in PDF, EPUB and Kindle. Book excerpt: The lee-surface flow phenomena on a delta-wing orbiter and a straight-wing orbiter have been investigated at angles of attack between 0 deg and 50 deg at a Mach number of 6. Limited studies of the delta-wing orbiter were conducted at a Mach number of 19. Heat-transfer data, pressure distributions, and oil-flow studies were employed to experimentally examine the nature of the surface flow and the severity of the lee-surface heating. The effects of Reynolds number on the flow field and heating were investigated. Problem areas are defined and areas for further study are recommended.

Book Heat Transfer and Flow Field Tests of the North American Rockwell  General Dynamics Convair Space Shuttle Configurations

Download or read book Heat Transfer and Flow Field Tests of the North American Rockwell General Dynamics Convair Space Shuttle Configurations written by and published by . This book was released on 1973 with total page 0 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.

Book Monthly Catalogue  United States Public Documents

Download or read book Monthly Catalogue United States Public Documents written by and published by . This book was released on 1985 with total page 1426 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book NASA Technical Memorandum

Download or read book NASA Technical Memorandum written by and published by . This book was released on 1986 with total page 168 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Heat Transfer and Flow Field Tests of the McDonnell Douglas Martin Marietta Space Shuttle Configurations

Download or read book Heat Transfer and Flow Field Tests of the McDonnell Douglas Martin Marietta Space Shuttle Configurations written by and published by . This book was released on 1973 with total page 0 pages. Available in PDF, EPUB and Kindle. Book excerpt: Aerothermodynamic tests of Phase B space shuttle configurations proposed by McDonnell Douglas--Martin Marietta were conducted at Mach numbers 8 and 10.5. 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 analysis which includes leeside heating, windward shock angles and flow fields, windward surface heating, and boundary-layer transition.

Book Research and Technology Objectives and Plans Summary  RTOPS

Download or read book Research and Technology Objectives and Plans Summary RTOPS written by and published by . This book was released on 1985 with total page 192 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Columbia Accident Investigation Board Report

Download or read book Columbia Accident Investigation Board Report written by United States. Columbia Accident Investigation Board and published by . This book was released on 2003 with total page 690 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Monthly Catalog of United States Government Publications

Download or read book Monthly Catalog of United States Government Publications written by United States. Superintendent of Documents and published by . This book was released on 1985 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt: February issue includes Appendix entitled Directory of United States Government periodicals and subscription publications; September issue includes List of depository libraries; June and December issues include semiannual index

Book NASA Technical Note

    Book Details:
  • Author :
  • Publisher :
  • Release : 1972
  • ISBN :
  • Pages : 420 pages

Download or read book NASA Technical Note written by and published by . This book was released on 1972 with total page 420 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Space Shuttle Aerothermodynamics Technology Conference  Held at Ames Research Center  Moffett Field  Calif   December 15 16  1971

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 278 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book An Experimental Investigation to Determine the Effect of Window Cooling by Mass Injection for the Shuttle Infrared Leeside Temperature Sensing  SILTS  Experiment

Download or read book An Experimental Investigation to Determine the Effect of Window Cooling by Mass Injection for the Shuttle Infrared Leeside Temperature Sensing SILTS Experiment written by and published by . This book was released on 1979 with total page 48 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book NASA Technical Paper

Download or read book NASA Technical Paper written by and published by . This book was released on 1980 with total page 82 pages. Available in PDF, EPUB and Kindle. Book excerpt: