Experimental Investigation of Generic Three-dimensional Sidewall-compression Scramjet Inlets at Mach 6 in Tetrafluoromethane

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Total Pages : 52 pages
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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:

Experimental Investigation of Generic Three-Dimensional Sidewall-Compression Scramjet Inlets at Mach 6 in Tetrafluoromethane

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Publisher : Createspace Independent Publishing Platform
ISBN 13 : 9781722219024
Total Pages : 48 pages
Book Rating : 4.2/5 (19 download)

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Book Synopsis Experimental Investigation of Generic Three-Dimensional Sidewall-Compression Scramjet Inlets at Mach 6 in Tetrafluoromethane by : National Aeronautics and Space Administration (NASA)

Download or read book Experimental Investigation of Generic Three-Dimensional Sidewall-Compression Scramjet Inlets at Mach 6 in Tetrafluoromethane 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 48 pages. Available in PDF, EPUB and Kindle. Book excerpt: Three-dimensional sidewall-compression scramjet inlets with leading-edge sweeps of 30 deg and 70 deg were tested in the Langley Hypersonic CF4 Tunnel at Mach 6 and with a ratio of specific heats of 1.2. The parametric effects of leading-edge sweep, cowl position, contraction ratio, and Reynolds number were investigated. The models were instrumented with 42 static pressure orifices that were distributed on the sidewalls, base plate, and cowl. Schlieren movies were made of each test for flow visualization of the effects of the internal flow spillage on the external flow field. To obtain an approximate characterization of the flow field, a modification to two-dimensional, inviscid, oblique shock theory was derived to accommodate the three-dimensional effects of leading-edge sweep. This theory qualitatively predicted the reflected shock structure (i.e., sidewall impingement locations) and the observed increase in spillage with increasing leading-edge sweep. The primary effect of moving the cowl forward was capturing the flow that would have otherwise spilled out ahead of the cowl. Increasing the contraction ratio increases the number of internal shock reflections and hence incrementally increases the sidewall pressure distribution. Significant Reynolds number effects were noted over a small range of Reynolds number. Holland, Scott D. Langley Research Center RTOP 506-40-41-02...

Contraction Ratio Effects in a Generic Three-dimensional Sidewall Compression Scramjet Inlet

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Book Synopsis Contraction Ratio Effects in a Generic Three-dimensional Sidewall Compression Scramjet Inlet by : Scott D. Holland

Download or read book Contraction Ratio Effects in a Generic Three-dimensional Sidewall Compression Scramjet Inlet written by Scott D. Holland and published by . This book was released on 1991 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:

Internal Aerodynamics of a Generic Three-dimensional Scramjet Inlet at Mach 10

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ISBN 13 :
Total Pages : 60 pages
Book Rating : 4.:/5 (317 download)

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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:

Monthly Catalog of United States Government Publications

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Scientific and Technical Aerospace Reports

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Total Pages : 772 pages
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Mach 10 Computational Study of a Three-dimensional Scramjet Inlet Flow Field

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Total Pages : 36 pages
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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:

The Scramjet Engine

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Publisher : Cambridge University Press
ISBN 13 : 1139478192
Total Pages : 271 pages
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An Experimental Parametric Study of Geometric, Reynolds Number and Ratio of Specific Heats Effects in Three-dimensional Sidewall Compression Scramjet Inlets at Mach 6

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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:

Computational Parametric Study of Sidewall-compression Scramjet Inlet Performance at Mach 10

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Total Pages : 20 pages
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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:

Monthly Catalogue, United States Public Documents

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Total Pages : 752 pages
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World Wide Web Implementation of the Langley Technical Report Server

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Total Pages : 36 pages
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Download or read book World Wide Web Implementation of the Langley Technical Report Server written by and published by . This book was released on 1994 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt:

30th Aerospace Sciences Meeting and Exhibit: 92-0670 - 92-0719

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Total Pages : 566 pages
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Reynolds Number and Cowl Position Effects for a Generic Sidewall Compression Scramjet Inlet at Mach 10

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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:

AIAA 22nd Fluid Dynamics, Plasma Dynamics & Lasers Conference: 91-1701 - 91-1749

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ISBN 13 :
Total Pages : 508 pages
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Download or read book AIAA 22nd Fluid Dynamics, Plasma Dynamics & Lasers Conference: 91-1701 - 91-1749 written by and published by . This book was released on 1991 with total page 508 pages. Available in PDF, EPUB and Kindle. Book excerpt:

41st AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit 10-13 July 2005, Tucson, Arizona

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Total Pages : 572 pages
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Aeronautical Engineering

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Total Pages : 932 pages
Book Rating : 4.:/5 (31 download)

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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).