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Results Of Ramjet Facility Model Tests At Mach 7
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Book Synopsis RESULTS OF RAMJET FACILITY MODEL TESTS AT MACH 7 by :
Download or read book RESULTS OF RAMJET FACILITY MODEL TESTS AT MACH 7 written by and published by . This book was released on 1963 with total page 105 pages. Available in PDF, EPUB and Kindle. Book excerpt: A test program was conducted to provide ramjet test facility bypass flow second throat diffuser pressure recovery data at a nominal nozzle exit Mach number of 7.0. During the tests a study was made of the effects of stagnation temperature, Reynolds number, ramjet inlet to facility nozzle exit area ratio, and other geometric variables. Two facility models were tested, the earlier Phase I model having a cowl lip angle of 35 degrees with a flare angle of 30 degrees, and the Phase II model having a lip and flare angle of 15 degrees. Prior to the tests it was hoped that it would be possible to attain bypass diffuser pressure recoveries approaching the pressure recovery across a normal shock at the nozzle exit Mach number. The best performance, which was obtained with the Phase II model, gave a pressure recovery corresponding to 65% of normal shock recovery. A significant influence of cowl flare angle was noted since the maximum recovery obtained with the Phase I model was 37% of normal shock recovery.
Book Synopsis Results of Ramjet Facility Model Tests at Mach 11 by : James L. Grunnet
Download or read book Results of Ramjet Facility Model Tests at Mach 11 written by James L. Grunnet and published by . This book was released on 1966 with total page 50 pages. Available in PDF, EPUB and Kindle. Book excerpt: A test program was conducted to provide ramjet test facility bypass flow second throat diffusers pressure recovery data at a nominal nozzle exit Mach number of 11.0. During the tests, studies were made to determine the effects of Reynolds number, diffuser throat length, inlet capture, area, and other variables. The pressure recoveries obtained during the testing proved to be somewhat better than the original expectations. The peak junning pressure recovery was over 60% of free stream normal shock recovery with the adjustable diffuser. Starting pressure recoveries were somewhat lower and ranged mostly from 20% to 30% of normal shock. (Author).
Book Synopsis U.S. Government Research Reports by :
Download or read book U.S. Government Research Reports written by and published by . This book was released on 1963 with total page 768 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis U.S. Government Research Reports by :
Download or read book U.S. Government Research Reports written by and published by . This book was released on 1963 with total page 1322 pages. Available in PDF, EPUB and Kindle. Book excerpt:
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Download or read book Scientific and Technical Aerospace Reports written by and published by . This book was released on 1995 with total page 464 pages. Available in PDF, EPUB and Kindle. Book excerpt:
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Download or read book NASA Technical Memorandum written by and published by . This book was released on 1980 with total page 648 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author :United States. Congress. House. Committee on Appropriations. Subcommittee on HUD-Independent Agencies Publisher : ISBN 13 : Total Pages :1072 pages Book Rating :4.:/5 (42 download)
Book Synopsis Department of Housing and Urban Development--independent agencies appropriations for 1987 by : United States. Congress. House. Committee on Appropriations. Subcommittee on HUD-Independent Agencies
Download or read book Department of Housing and Urban Development--independent agencies appropriations for 1987 written by United States. Congress. House. Committee on Appropriations. Subcommittee on HUD-Independent Agencies and published by . This book was released on 1986 with total page 1072 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Operating Characteristics of the Langley Mach 7 Scramjet Test Facility by :
Download or read book Operating Characteristics of the Langley Mach 7 Scramjet Test Facility written by and published by . This book was released on 1981 with total page 60 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book NASA Technical Paper written by and published by . This book was released on 1983 with total page 492 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis 17th JANNAF Combustion Meeting, NASA Langley Research Center, Hampton, Virginia, September 22-26, 1980 by :
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Book Synopsis Bibliography of Scientific and Industrial Reports by :
Download or read book Bibliography of Scientific and Industrial Reports written by and published by . This book was released on 1970 with total page 870 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Ramjet Engines by : Mikhail Makarovich Bondari͡u︡k
Download or read book Ramjet Engines written by Mikhail Makarovich Bondari͡u︡k and published by . This book was released on 1969 with total page 466 pages. Available in PDF, EPUB and Kindle. Book excerpt:
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Download or read book NASA Scientific and Technical Publications written by and published by . This book was released on 1987 with total page 410 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Expanded Operational Capabilities of the Langley Mach 7 Scramjet Test Facility by : Scott R. Thomas
Download or read book Expanded Operational Capabilities of the Langley Mach 7 Scramjet Test Facility written by Scott R. Thomas and published by . This book was released on 1983 with total page 80 pages. Available in PDF, EPUB and Kindle. Book excerpt:
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Download or read book Research and Technology Program Digest Flash Index written by and published by . This book was released on 1967 with total page 794 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis 36th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit: 2000-3600 - 2000-3649 by :
Download or read book 36th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit: 2000-3600 - 2000-3649 written by and published by . This book was released on 2000 with total page 552 pages. Available in PDF, EPUB and Kindle. Book excerpt:
