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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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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Book Description


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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Monthly Catalogue, United States Public Documents

Monthly Catalogue, United States Public Documents PDF Author:
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 944

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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 : 1632

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Mach 10 Experimental Database of a Three-dimensional Scramjet Inlet Flow Field

Mach 10 Experimental Database of a Three-dimensional Scramjet Inlet Flow Field PDF Author: Scott Douglas Holland
Publisher:
ISBN:
Category : Aerodynamics, Hypersonic
Languages : en
Pages : 226

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Scientific and Technical Aerospace Reports

Scientific and Technical Aerospace Reports PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 704

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Hypersonic Curved Compression Inlet and Its Inverse Design

Hypersonic Curved Compression Inlet and Its Inverse Design PDF Author: Kunyuan Zhang
Publisher: Springer Nature
ISBN: 9811507279
Category : Science
Languages : en
Pages : 340

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Book Description
This book presents systematic research results on curved shock wave-curved compression surface applied to the compression surface design of supersonic–hypersonic inlet, which is a brand new inlet design. The concept of supersonic inlet curved compression discussed originated from the author’s research at the Deutsches Zentrum fur Luft- und Raumfahrt (DLR SM-ES) in the early 1990s. This book introduces the research history, working characteristics, performance calculation and aerodynamic configuration design method of this compression mode in detail. It also describes method of estimating the minimum drag in inlet and drag reduction effect of curved compression and proposes a new index for evaluating unit area compression efficiency of the inlet. Further, it reviews the relevant recent research on curved compression. As such it is a valuable resource for students, researchers and scientists in the fields of hypersonic propulsion and aeronautics.

NASA Aerodynamics Program, Annual Report 1991

NASA Aerodynamics Program, Annual Report 1991 PDF Author:
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 262

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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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NASA Langley Scientific and Technical Information Output, 1995

NASA Langley Scientific and Technical Information Output, 1995 PDF Author:
Publisher:
ISBN:
Category : Astronautics
Languages : en
Pages : 172

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Book Description
This document is a compilation of the scientific and technical information that the Langley Research Center has produced during the calendar year 1995. Included are citations for formal reports, high-numbered conference publications, high-numbered technical memorandums, contractor reports, journal articles and other publications, meeting presentations, technical talks, computer programs, tech briefs, and patents.