Author: Scott D. Holland
Publisher:
ISBN:
Category : Aerothermodynamics
Languages : en
Pages : 60
Book Description
Internal Aerodynamics of a Generic Three-dimensional Scramjet Inlet at Mach 10
Author: Scott D. Holland
Publisher:
ISBN:
Category : Aerothermodynamics
Languages : en
Pages : 60
Book Description
Publisher:
ISBN:
Category : Aerothermodynamics
Languages : en
Pages : 60
Book Description
Mach 10 Computational Study of a Three-dimensional Scramjet Inlet Flow Field
Author: Scott D. Holland
Publisher:
ISBN:
Category :
Languages : en
Pages : 36
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 36
Book Description
Monthly Catalogue, United States Public Documents
Author:
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 944
Book Description
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 944
Book Description
Monthly Catalog of United States Government Publications
Author:
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1632
Book Description
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1632
Book Description
Mach 10 Experimental Database of a Three-dimensional Scramjet Inlet Flow Field
Author: Scott Douglas Holland
Publisher:
ISBN:
Category : Aerodynamics, Hypersonic
Languages : en
Pages : 226
Book Description
Publisher:
ISBN:
Category : Aerodynamics, Hypersonic
Languages : en
Pages : 226
Book Description
Scientific and Technical Aerospace Reports
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 704
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 704
Book Description
Hypersonic Curved Compression Inlet and Its Inverse Design
Author: Kunyuan Zhang
Publisher: Springer Nature
ISBN: 9811507279
Category : Science
Languages : en
Pages : 340
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.
Publisher: Springer Nature
ISBN: 9811507279
Category : Science
Languages : en
Pages : 340
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
Author:
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 262
Book Description
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 262
Book Description
Computational Parametric Study of Sidewall-compression Scramjet Inlet Performance at Mach 10
Author: Scott D. Holland
Publisher:
ISBN:
Category :
Languages : en
Pages : 20
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 20
Book Description
NASA Langley Scientific and Technical Information Output, 1995
Author:
Publisher:
ISBN:
Category : Astronautics
Languages : en
Pages : 172
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.
Publisher:
ISBN:
Category : Astronautics
Languages : en
Pages : 172
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.