Download or read book Magnetohydrodynamics Accelerator Research Into Advanced Hypersonics Mariah written by National Aeronautics and Space Administration (NASA) and published by Createspace Independent Publishing Platform. This book was released on 2018-07-27 with total page 436 pages. Available in PDF, EPUB and Kindle. Book excerpt: This report documents the activities, results, conclusions and recommendations of the Magnetohydrodynamics Accelerator Research Into Advanced Hypersonics (MARIAH) Project in which the use of magnetohydrodynamics (MHD) technology is investigated for its applicability to augment hypersonic wind tunnels. The long range objective of this investigation is to advance the development of ground test facilities to support the development of hypervelocity flight vehicles. The MHD accelerator adds kinetic energy directly to the wind tunnel working fluid, thereby increasing its Mach number to hypervelocity levels. Several techniques for MHD augmentation, as well as other physical characteristics of the process are studied to enhance the overall performance of hypersonic wind tunnel design. Specific recommendations are presented to improve the effectiveness of ground test facilities. The work contained herein builds on nearly four decades of research and experimentation by the aeronautics ground test and evaluation community, both foreign and domestic. Baughman, Jack A. and Micheletti, David A. and Nelson, Gordon L. and Simmons, Gloyd A. Langley Research Center NASA/CR-97-206242-Pt-2, NAS 1.26:206242-Pt-2, MSE-029-Pt-2 DE-AC22-96EW-96405; NASA Order A-45416-D...
Download or read book Magnetohydrodynamics Accelerator Research Into Advanced Hypersonics MARIAH written by and published by . This book was released on 1997 with total page 658 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Magnetohydrodynamics Accelerator Research Into Advanced Hypersonics MARIAH written by and published by . This book was released on 1997 with total page 444 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book MAGNETOHYDRODYNAMICS ACCELERATOR RESEARCH INTO ADVANCED HYPERSONICS MARIAH FINAL REPORT NASA CR 97 206242 PT 2 DEC 30 1997 written by United States. National Aeronautics and Space Administration and published by . This book was released on 1998* with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book MAGNETOHYDRODYNAMICS ACCELERATOR RESEARCH INTO ADVANCED HYPERSONICS MARIAH FINAL REPORT NASA CR 97 206424 PT 1 DEC 30 1997 written by United States. National Aeronautics and Space Administration and published by . This book was released on 1998* with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Radiatively Driven Hypersonic Wind Tunnel RDHWT Program Magnetohydrodynamic Accelerator Research Into Advanced Hypersonics MARIAH II written by and published by . This book was released on 2000 with total page 335 pages. Available in PDF, EPUB and Kindle. Book excerpt: This report documents the first year's progress on the research for the development of enabling technology for the design of a Mach 8-15 flight duplication wind tunnel. This research program is entitled the Radiantly Driven Hypersonic Wind Tunnel/Magnetohydrodynamics Accelerator Research Into Advanced Hypersonics (RDHWT/MARIAH II) program. Direction of the program is provided by the USAF Arnold Engineering Development Center (AEDC). MSE Technology Applications, Inc. (MSE) is serving as the program prime integrating contractor. Other key team members include the U.S. Department of Energy Federal Energy Technology Center (DOE-FETC), Lawrence Livermore National Laboratory (LLNL), Sandia National Laboratories (SNL), and Princeton University.
Download or read book Magnetohydrodynamics Accelerator Research Into Advanced Hypersonics MARIAH written by Jack A. Baughman and published by . This book was released on 1997 with total page 405 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book RDHWT MARIAH II Hypersonic Wind Tunnel Research Program written by and published by . This book was released on 2008 with total page 165 pages. Available in PDF, EPUB and Kindle. Book excerpt: The U.S. Air Force sponsored and the USAF Arnold Engineering Development Center directed the Radiantly Driven Hypersonic Wind Tunnel (RDHWT)/ Magnetohydrodynamic Accelerator Research Into Advanced Hypersonics (MARIAH II) Program. This report primarily covers the research for the period from January 2001 through July 2004. The scope of the research program was to develop enabling technologies for a medium-scale hypersonic wind tunnel (MSHWT) that would provide a Mach 8 to 15 test capability with aeropropulsion testing as the principal need and focus. The USAF research program has been terminated, but work continues under Army sponsorship. Considerable progress has been achieved, and this final report summarizes the work. Key participants in this work were MSE Technology Applications, Inc., the prime integrating contractor; Princeton University; Ring Technical Services (RTS); Lawrence Livermore National Laboratory (LLNL); Sandia National Laboratory (SNL); and Oak Ridge National Laboratory (ORNL) (funded by a separate DoD program).
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:
Download or read book Engineering Aspects of Magnetohydrodynamics written by and published by . This book was released on 1995 with total page 596 pages. Available in PDF, EPUB and Kindle. Book excerpt:
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Download or read book Potential Application of Magnetohydrodynamic Acceleration to Hypersonic Environmental Testing written by and published by . This book was released on 1990 with total page 97 pages. Available in PDF, EPUB and Kindle. Book excerpt: This investigation reviews the technical results from previous MHD accelerator research and conducts a theoretical analysis of the simulation capabilities of an MHD-augmented hypersonic flow facility. This investigation identified the performance potential of MHD accelerator and hot gas generator combinations subject to reasonable constraints from available technology. The performance goal was to extend the hypersonic flight simulation limits from Mach 10 to Mach 25. The results of this investigation identified the critical technology issues which must be addressed in the design of an MHD-driven hypersonic test facility.
Download or read book 34th AIAA ASME SAE ASEE Joint Propulsion Conference Exhibit written by and published by . This book was released on 1998 with total page 636 pages. Available in PDF, EPUB and Kindle. Book excerpt:
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Download or read book 35th AIAA ASME SAE ASEE Joint Propulsion Conference and Exhibit written by and published by . This book was released on 1999 with total page 530 pages. Available in PDF, EPUB and Kindle. Book excerpt:
