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Computational Parametric Study Of Sidewall Compression Scramjet Inlet Performance At Mach 10
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Book Synopsis Computational Parametric Study of Sidewall-compression Scramjet Inlet Performance at Mach 10 by : Scott D. Holland
Download or read book Computational Parametric Study of Sidewall-compression Scramjet Inlet Performance at Mach 10 written by Scott D. Holland and published by . This book was released on 1993 with total page 20 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Computational Parametric Study of Sidewall-compression Scramjet Inlet Performance at Mach 10 by : Scott Douglas Holland
Download or read book Computational Parametric Study of Sidewall-compression Scramjet Inlet Performance at Mach 10 written by Scott Douglas Holland and published by . This book was released on 1993 with total page 11 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis A Computational Parametric Study of Three-dimensional Sidewall Compression Scramjet Inlets at Mach 10 by : Scott D. Holland
Download or read book A Computational Parametric Study of Three-dimensional Sidewall Compression Scramjet Inlets at Mach 10 written by Scott D. Holland and published by . This book was released on 1990 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Mach 10 Computational Study of a Three-dimensional Scramjet Inlet Flow Field by : Scott D. Holland
Download or read book Mach 10 Computational Study of a Three-dimensional Scramjet Inlet Flow Field written by Scott D. Holland and published by . This book was released on 1995 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Internal Aerodynamics of a Generic Three-dimensional Scramjet Inlet at Mach 10 by : Scott D. Holland
Download or read book Internal Aerodynamics of a Generic Three-dimensional Scramjet Inlet at Mach 10 written by Scott D. Holland and published by . This book was released on 1995 with total page 60 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author :National Aeronautics and Space Administration (NASA) Publisher :Createspace Independent Publishing Platform ISBN 13 :9781722351687 Total Pages :32 pages Book Rating :4.3/5 (516 download)
Book Synopsis Mach 10 Computational Study of a Three-Dimensional Scramjet Inlet Flow Field by : National Aeronautics and Space Administration (NASA)
Download or read book Mach 10 Computational Study of a Three-Dimensional Scramjet Inlet Flow Field written by National Aeronautics and Space Administration (NASA) and published by Createspace Independent Publishing Platform. This book was released on 2018-07-05 with total page 32 pages. Available in PDF, EPUB and Kindle. Book excerpt: The present work documents the computational results for a combined computational and experimental parametric study of the internal aerodynamics of a generic three-dimensional sidewall-compression scramjet inlet configuration at Mach 10. The three-dimensional Navier-Stokes code SCRAMIN was chosen for the computational portion of the study because it uses a well-known and well-proven numerical scheme and has shown favorable comparison with experiment at Mach numbers between 2 and 6. One advantage of CFD was that it provided flow field data for a detailed examination of the internal flow characteristics in addition to the surface properties. The experimental test matrix at mach 10 included three geometric contraction ratios (3, 5, and 9), three Reynolds numbers (0.55 x 10(exp 6) per foot, 1.14 x 10(exp 6) per foot, and 2.15 x 10(exp 6) per foot), and three cowl positions (at the throat and two forward positions). Computational data for two of these configurations (the contraction ratio of 3, Re = 2.15 x 10 (exp 6) per foot, at two cowl positions) are presented along with a detailed analysis of the flow interactions in successive computational planes. Holland, Scott D. Langley Research Center RTOP 506-40-41-02...
Author :National Aeronautics and Space Administration (NASA) Publisher :Createspace Independent Publishing Platform ISBN 13 :9781724289414 Total Pages :220 pages Book Rating :4.2/5 (894 download)
Book Synopsis Mach 10 Experimental Database of a Three-Dimensional Scramjet Inlet Flow Field by : National Aeronautics and Space Administration (NASA)
Download or read book Mach 10 Experimental Database of a Three-Dimensional Scramjet Inlet Flow Field 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 220 pages. Available in PDF, EPUB and Kindle. Book excerpt: The present work documents the experimental database of a combined computational and experimental parametric study of the internal aerodynamics of a generic three-dimensional sidewall compression scramjet inlet configuration at Mach 10. A total of 356 channels of pressure data, including static pressure orifices, pitot pressures, and exit flow rakes, along with oil flow and infrared thermography, provided a detailed experimental description of the flow. Mach 10 tests were performed for three geometric contraction ratios (3, 5, and 9), three Reynolds numbers (0.55 x 10(exp 6) per foot, 1.14 x 10(exp 6) per foot, and 2.15 x 10(exp 6) per foot), and three cowl positions (at the throat and two forward positions). For the higher contraction ratios, a large forward separation of the inflow boundary layer was observed, making the high contraction ratio configurations unsuitable for flight operation. A decrease in the freestream unit Reynolds number (Re) of only a factor of 2 led to a similar upstream separation. Although the presence of such large-scale separations leads to the question of whether the inlet is started, the presence of internal oblique swept shock interactions on the sidewalls seems to indicate that at least in the classical sense, the inlet is not unstarted. The laminar inflow boundary layer therefore appears to be very sensitive to increases in contraction ratio (CR) or decreases in Reynolds number; only the CR = 3 configuration with 0.25, and 50 percent cowl at Re = 2.15 x 10(exp 6) per foot operated 'on design'. Holland, Scott D. Langley Research Center NASA-TM-4648, L-17349, NAS 1.15:4648 RTOP 506-40-41-02...
Book Synopsis Reynolds Number and Cowl Position Effects for a Generic Sidewall Compression Scramjet Inlet at Mach 10 by : Scott D. Holland
Download or read book Reynolds Number and Cowl Position Effects for a Generic Sidewall Compression Scramjet Inlet at Mach 10 written by Scott D. Holland and published by . This book was released on 1992 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Computational Simulation of a Three-dimensional Scramjet Inlet Flow Field at Mach 10 by : Fangrong Ye
Download or read book Computational Simulation of a Three-dimensional Scramjet Inlet Flow Field at Mach 10 written by Fangrong Ye and published by . This book was released on 1999 with total page 176 pages. Available in PDF, EPUB and Kindle. Book excerpt: "The present work documents the results of computational simulation of three-dimensional sidewall-compression scramjet inlet configurations at Mach 10." (i).
Book Synopsis An Experimental Parametric Study of Geometric, Reynolds Number and Ratio of Specific Heats Effects in Three-dimensional Sidewall Compression Scramjet Inlets at Mach 6 by : Scott D. Holland
Download or read book An Experimental Parametric Study of Geometric, Reynolds Number and Ratio of Specific Heats Effects in Three-dimensional Sidewall Compression Scramjet Inlets at Mach 6 written by Scott D. Holland and published by . This book was released on 1993 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Experimental Investigation of Generic Three-dimensional Sidewall-compression Scramjet Inlets at Mach 6 in Tetrafluoromethane by : Scott D. Holland
Download or read book Experimental Investigation of Generic Three-dimensional Sidewall-compression Scramjet Inlets at Mach 6 in Tetrafluoromethane written by Scott D. Holland and published by . This book was released on 1993 with total page 52 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 1995 with total page 538 pages. Available in PDF, EPUB and Kindle. Book excerpt: Lists citations with abstracts for aerospace related reports obtained from world wide sources and announces documents that have recently been entered into the NASA Scientific and Technical Information Database.
Book Synopsis Aeronautical Engineering: A Cumulative Index to a Continuing Bibliography (supplement 300) by :
Download or read book Aeronautical Engineering: A Cumulative Index to a Continuing Bibliography (supplement 300) written by and published by . This book was released on 1994 with total page 686 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis 29th International Symposium on Shock Waves 1 by : Riccardo Bonazza
Download or read book 29th International Symposium on Shock Waves 1 written by Riccardo Bonazza and published by Springer. This book was released on 2015-07-09 with total page 832 pages. Available in PDF, EPUB and Kindle. Book excerpt: This proceedings present the results of the 29th International Symposium on Shock Waves (ISSW29) which was held in Madison, Wisconsin, U.S.A., from July 14 to July 19, 2013. It was organized by the Wisconsin Shock Tube Laboratory, which is part of the College of Engineering of the University of Wisconsin-Madison. The ISSW29 focused on the following areas: Blast Waves, Chemically Reactive Flows, Detonation and Combustion, Facilities, Flow Visualization, Hypersonic Flow, Ignition, Impact and Compaction, Industrial Applications, Magnetohydrodynamics, Medical and Biological Applications, Nozzle Flow, Numerical Methods, Plasmas, Propulsion, Richtmyer-Meshkov Instability, Shock-Boundary Layer Interaction, Shock Propagation and Reflection, Shock Vortex Interaction, Shock Waves in Condensed Matter, Shock Waves in Multiphase Flow, as well as Shock Waves in Rarefield Flow. The two Volumes contain the papers presented at the symposium and serve as a reference for the participants of the ISSW 29 and individuals interested in these fields.
Book Synopsis Scramjet Propulsion by : E. T. Curran
Download or read book Scramjet Propulsion written by E. T. Curran and published by AIAA. This book was released on 2001 with total page 1354 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Hypersonic Airbreathing Propulsion by : William H. Heiser
Download or read book Hypersonic Airbreathing Propulsion written by William H. Heiser and published by AIAA. This book was released on 1994 with total page 632 pages. Available in PDF, EPUB and Kindle. Book excerpt: An almost entirely self-contained engineering textbook primarily for use in undergraduate and graduate courses in airbreathing propulsion. It provides a broad and basic introduction to the elements needed to work in the field as it develops and grows. Homework problems are provided for almost every individual subject. An extensive array of PC-based user-friendly computer programs is provided in order to facilitate repetitious and/or complex calculations. Annotation copyright by Book News, Inc., Portland, OR
Download or read book Aeronautical Engineering written by and published by . This book was released on 1993 with total page 932 pages. Available in PDF, EPUB and Kindle. Book excerpt: A selection of annotated references to unclassified reports and journal articles that were introduced into the NASA scientific and technical information system and announced in Scientific and technical aerospace reports (STAR) and International aerospace abstracts (IAA).
