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Modification To The Langley 8 Foot High Temperature Tunnel For Hypersonic Propulsion Testing
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Book Synopsis Modification to the Langley 8-foot High Temperature Tunnel for Hypersonic Propulsion Testing by : D. E. Reubush
Download or read book Modification to the Langley 8-foot High Temperature Tunnel for Hypersonic Propulsion Testing written by D. E. Reubush and published by . This book was released on 1987 with total page 16 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Modification of NASA Langley 8 Foot High Temperature Tunnel to Provide a Unique National Research Facility for Hypersonic Air-breathing Propulsion Systems by :
Download or read book Modification of NASA Langley 8 Foot High Temperature Tunnel to Provide a Unique National Research Facility for Hypersonic Air-breathing Propulsion Systems written by and published by . This book was released on 1984 with total page 14 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author :National Aeronautics and Space Administration (NASA) Publisher :Createspace Independent Publishing Platform ISBN 13 :9781724731869 Total Pages :28 pages Book Rating :4.7/5 (318 download)
Book Synopsis Support of the Eight-Foot High Temperature Tunnel Modification Project by : National Aeronautics and Space Administration (NASA)
Download or read book Support of the Eight-Foot High Temperature Tunnel Modification Project written by National Aeronautics and Space Administration (NASA) and published by Createspace Independent Publishing Platform. This book was released on 2018-08-06 with total page 28 pages. Available in PDF, EPUB and Kindle. Book excerpt: In order to meet the need for propulsion testing in the high supersonic range from Mach 4 to Mach 7, NASA has undertaken the modification of the Langley Eight Foot High Temperature Tunnel to add alternate Mach number capability and oxygen enrichment to allow the testing of operating engines at these Mach numbers and at true temperature tunnel. The transfer of liquid oxygen (LOX) from a storage vessel to a rocket engine generally requires the use of a pressurizing gas at high pressures. Although nitrogen is preferred, unfortunately, when gaseous nitrogen (GN2) is used as the pressurant to transfer liquid oxygen from a storage tank to the tunnel combustor, it contaminates the liquid oxygen and effects a loss of performance in the engine. The contamination of the LOX by the pressurizing GN2 is described, which may prove to be an important operational constraint. It is desirable to have reliable data concerning the penetration of GN2 into LOX during pressurization and the subsequent of self cleaning after blowdown. Ngo, Kim Chi and Mielke, Roland R. Unspecified Center NASA-CR-181280, NAS 1.26:181280 NAS1-17993
Book Synopsis Calibration of the Langley 8-foot High Temperature Tunnel for Hypersonic Air-breathing Propulsion Testing by : Lawrence D. Huebner
Download or read book Calibration of the Langley 8-foot High Temperature Tunnel for Hypersonic Air-breathing Propulsion Testing written by Lawrence D. Huebner and published by . This book was released on 1996 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Hyper-X Engine Testing in the NASA Langley 8-foot High-temperature Tunnel by : Lawrence D. Huebner
Download or read book Hyper-X Engine Testing in the NASA Langley 8-foot High-temperature Tunnel written by Lawrence D. Huebner and published by . This book was released on 2000 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Test Capabilities and Recent Experiences in the NASA Langley 8-foot High Temperature Tunnel by : Jeffrey S. Hodge
Download or read book Test Capabilities and Recent Experiences in the NASA Langley 8-foot High Temperature Tunnel written by Jeffrey S. Hodge and published by . This book was released on 2000 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author :National Aeronautics and Space Administration (NASA) Publisher :Createspace Independent Publishing Platform ISBN 13 :9781722118709 Total Pages :38 pages Book Rating :4.1/5 (187 download)
Book Synopsis Computational Method to Predict Thermodynamic, Transport, and Flow Properties for the Modified Langley 8-Foot High-Temperature Tunnel by : National Aeronautics and Space Administration (NASA)
Download or read book Computational Method to Predict Thermodynamic, Transport, and Flow Properties for the Modified Langley 8-Foot High-Temperature Tunnel written by National Aeronautics and Space Administration (NASA) and published by Createspace Independent Publishing Platform. This book was released on 2018-07-02 with total page 38 pages. Available in PDF, EPUB and Kindle. Book excerpt: The Langley 8 foot high temperature tunnel (8 ft HTT) is used to test components of hypersonic vehicles for aerothermal loads definition and structural component verification. The test medium of the 8 ft HTT is obtained by burning a mixture of methane and air under high pressure; the combustion products are expanded through an axisymmetric conical contoured nozzle to simulate atmospheric flight at Mach 7. This facility was modified to raise the oxygen content of the test medium to match that of air and to include Mach 4 and Mach 5 capabilities. These modifications will facilitate the testing of hypersonic air breathing propulsion systems for a wide range of flight conditions. A computational method to predict the thermodynamic, transport, and flow properties of the equilibrium chemically reacting oxygen enriched methane-air combustion products was implemented in a computer code. This code calculates the fuel, air, and oxygen mass flow rates and test section flow properties for Mach 7, 5, and 4 nozzle configurations for given combustor and mixer conditions. Salient features of the 8 ft HTT are described, and some of the predicted tunnel operational characteristics are presented in the carpet plots to assist users in preparing test plans. Venkateswaran, S. and Hunt, L. Roane and Prabhu, Ramadas K. Langley Research Center RTOP 506-43-31-05...
Book Synopsis Total Temperature Probes for High-temperature Hypersonic Boundary-layer Measurements by : Cindy W. Albertson
Download or read book Total Temperature Probes for High-temperature Hypersonic Boundary-layer Measurements written by Cindy W. Albertson and published by . This book was released on 1993 with total page 40 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Computational Method to Predict Thermodynamic, Transport, and Flow Properties for the Modified Langley 8-foot High-temperature Tunnel by : S. Venkateswaran
Download or read book Computational Method to Predict Thermodynamic, Transport, and Flow Properties for the Modified Langley 8-foot High-temperature Tunnel written by S. Venkateswaran and published by . This book was released on 1992 with total page 40 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Computational Method to Predict Thermodynamic, Transport, and Flow Properties for the Modified Langley 8-foot High-temperature Tunnel by : S. Venkateswaran
Download or read book Computational Method to Predict Thermodynamic, Transport, and Flow Properties for the Modified Langley 8-foot High-temperature Tunnel written by S. Venkateswaran and published by . This book was released on 1992 with total page 40 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Wind-tunnel Investigation at Mach Numbers from 3.0 to 6.8 of the Static Aerodynamic Characteristics of Modified Mercury Exit and Escape Capsule Configurations by : Albin O. Pearson
Download or read book Wind-tunnel Investigation at Mach Numbers from 3.0 to 6.8 of the Static Aerodynamic Characteristics of Modified Mercury Exit and Escape Capsule Configurations written by Albin O. Pearson and published by . This book was released on 1960 with total page 26 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Characteristics of Major Active Wind Tunnels at the Langley Research Center by : William T. Jr Schaefer
Download or read book Characteristics of Major Active Wind Tunnels at the Langley Research Center written by William T. Jr Schaefer and published by . This book was released on 1965 with total page 52 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Advanced Hypersonic Test Facilities by : Frank K. Lu
Download or read book Advanced Hypersonic Test Facilities written by Frank K. Lu and published by AIAA. This book was released on 2002 with total page 694 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Description of a 2-foot Hypersonic Facility at the Langley Research Center by : George M. Stokes
Download or read book Description of a 2-foot Hypersonic Facility at the Langley Research Center written by George M. Stokes and published by . This book was released on 1961 with total page 28 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author :United States. Congress. House. Committee on Science, Space, and Technology. Subcommittee on Technology, Environment, and Aviation Publisher : ISBN 13 : Total Pages :110 pages Book Rating :4.F/5 ( download)
Book Synopsis Enhancing U.S. Competitiveness by : United States. Congress. House. Committee on Science, Space, and Technology. Subcommittee on Technology, Environment, and Aviation
Download or read book Enhancing U.S. Competitiveness written by United States. Congress. House. Committee on Science, Space, and Technology. Subcommittee on Technology, Environment, and Aviation and published by . This book was released on 1994 with total page 110 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Support of the Eight-foot High Temperature Tunnel Modification Project by : Roland R. Mielke
Download or read book Support of the Eight-foot High Temperature Tunnel Modification Project written by Roland R. Mielke and published by . This book was released on 1987 with total page 20 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Description and Calibration of the Langley Hypersonic CF4 Tunnel by : Raymond E. Midden
Download or read book Description and Calibration of the Langley Hypersonic CF4 Tunnel written by Raymond E. Midden and published by . This book was released on 1985 with total page 84 pages. Available in PDF, EPUB and Kindle. Book excerpt:
