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

Experimental Investigation of Generic Three-dimensional Sidewall-compression Scramjet Inlets at Mach 6 in Tetrafluoromethane PDF Author: Scott D. Holland
Publisher:
ISBN:
Category : Aerodynamics, Hypersonic
Languages : en
Pages : 52

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

Experimental Investigation of Generic Three-dimensional Sidewall-compression Scramjet Inlets at Mach 6 in Tetrafluoromethane PDF Author: Scott D. Holland
Publisher:
ISBN:
Category : Aerodynamics, Hypersonic
Languages : en
Pages : 52

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

Experimental Investigation of Generic Three-Dimensional Sidewall-Compression Scramjet Inlets at Mach 6 in Tetrafluoromethane PDF Author: National Aeronautics and Space Administration (NASA)
Publisher: Createspace Independent Publishing Platform
ISBN: 9781722219024
Category :
Languages : en
Pages : 48

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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...

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

Internal Aerodynamics of a Generic Three-dimensional Scramjet Inlet at Mach 10 PDF Author: Scott D. Holland
Publisher:
ISBN:
Category : Aerothermodynamics
Languages : en
Pages : 60

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Scientific and Technical Aerospace Reports

Scientific and Technical Aerospace Reports PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 772

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Monthly Catalog of United States Government Publications

Monthly Catalog of United States Government Publications PDF Author:
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages :

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Mach 10 Computational Study of a Three-dimensional Scramjet Inlet Flow Field

Mach 10 Computational Study of a Three-dimensional Scramjet Inlet Flow Field PDF Author: Scott D. Holland
Publisher:
ISBN:
Category :
Languages : en
Pages : 36

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The Scramjet Engine

The Scramjet Engine PDF Author: Corin Segal
Publisher: Cambridge University Press
ISBN: 1139478192
Category : Technology & Engineering
Languages : en
Pages : 271

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Book Description
The renewed interest in high-speed propulsion has led to increased activity in the development of the supersonic combustion ramjet engine for hypersonic flight applications. In the hypersonic regime the scramjet engine's specific thrust exceeds that of other propulsion systems. This book, written by a leading researcher, describes the processes and characteristics of the scramjet engine in a unified manner, reviewing both theoretical and experimental research. The focus is on the phenomena that dictate the thermo-aerodynamic processes encountered in the scramjet engine, including component analyses and flowpath considerations; fundamental theoretical topics related to internal flow with chemical reactions and non-equilibrium effects, high-temperature gas dynamics, and hypersonic effects are included. Cycle and component analyses are further described, followed by flowpath examination. Finally, the book reviews experimental and theoretical capabilities and describes ground testing facilities and computational fluid dynamics facilities developed for the study of time-accurate, high-temperature aerodynamics.

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

Computational Parametric Study of Sidewall-compression Scramjet Inlet Performance at Mach 10 PDF Author: Scott D. Holland
Publisher:
ISBN:
Category :
Languages : en
Pages : 20

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Monthly Catalogue, United States Public Documents

Monthly Catalogue, United States Public Documents PDF Author:
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 752

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World Wide Web Implementation of the Langley Technical Report Server

World Wide Web Implementation of the Langley Technical Report Server PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 36

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