Author : Anonim
Publisher : Unknown
Page : 596 pages
File Size : 55,5 Mb
Release : 1992
Category : Electronic
ISBN : NASA:31769000472665
Performance Of Vortex Generators In A Mach 2 5 Low Bleed Full Scale 45 Percent Internal Contraction Axisymmetric Inlet
Performance Of Vortex Generators In A Mach 2 5 Low Bleed Full Scale 45 Percent Internal Contraction Axisymmetric Inlet Book in PDF, ePub and Kindle version is available to download in english. Read online anytime anywhere directly from your device. Click on the download button below to get a free pdf file of Performance Of Vortex Generators In A Mach 2 5 Low Bleed Full Scale 45 Percent Internal Contraction Axisymmetric Inlet book. This book definitely worth reading, it is an incredibly well-written.
NASA Technical Memorandum
Author : Anonim
Publisher : Unknown
Page : 882 pages
File Size : 47,5 Mb
Release : 1976
Category : Aeronautics
ISBN : UOM:39015040296553
NASA Technical Memorandum by Anonim Pdf
Performance of Vortex Generators in a Mach 2.5 Low-bleed Full-scale 45-percent-internal-contraction Axisymmetric Inlet
Author : Harvey E. Neumann
Publisher : Unknown
Page : 52 pages
File Size : 44,8 Mb
Release : 1975
Category : Aerodynamics, Supersonic
ISBN : UIUC:30112106566885
Performance of Vortex Generators in a Mach 2.5 Low-bleed Full-scale 45-percent-internal-contraction Axisymmetric Inlet by Harvey E. Neumann Pdf
Shock Waves
Author : Klaus Hannemann,Friedrich Seiler
Publisher : Springer Science & Business Media
Page : 810 pages
File Size : 49,6 Mb
Release : 2009-04-01
Category : Science
ISBN : 9783540851684
Shock Waves by Klaus Hannemann,Friedrich Seiler Pdf
The 26th International Symposium on Shock Waves in Göttingen, Germany was jointly organised by the German Aerospace Centre DLR and the French-German Research Institute of Saint Louis ISL. The year 2007 marked the 50th anniversary of the Symposium, which first took place in 1957 in Boston and has since become an internationally acclaimed series of meetings for the wider Shock Wave Community. The ISSW26 focused on the following areas: Shock Propagation and Reflection, Detonation and Combustion, Hypersonic Flow, Shock Boundary Layer Interaction, Numerical Methods, Medical, Biological and Industrial Applications, Richtmyer Meshkov Instability, Blast Waves, Chemically Reacting Flows, Diagnostics, Facilities, Flow Visualisation, Ignition, Impact and Compaction, Multiphase Flow, Nozzles Flows, Plasmas and Propulsion. The two Volumes contain the papers presented at the symposium and serve as a reference for the participants of the ISSW 26 and individuals interested in these fields.
Monthly Catalog of United States Government Publications
Author : Anonim
Publisher : Unknown
Page : 1126 pages
File Size : 40,8 Mb
Release : 1975
Category : Government publications
ISBN : STANFORD:36105119621071
Monthly Catalog of United States Government Publications by Anonim Pdf
NASA SP.
Author : Anonim
Publisher : Unknown
Page : 1066 pages
File Size : 40,5 Mb
Release : 1975
Category : Aeronautics
ISBN : MINN:319510005859970
NASA SP. by Anonim Pdf
Scientific and Technical Aerospace Reports
Author : Anonim
Publisher : Unknown
Page : 978 pages
File Size : 49,9 Mb
Release : 1975
Category : Aeronautics
ISBN : UVA:X004872598
Scientific and Technical Aerospace Reports by Anonim Pdf
Design of a Very-low-bleed Mach 2.5 Mixed-compression Inlet with 45 Percent Internal Contraction
Author : Joseph F. Wasserbauer
Publisher : Unknown
Page : 76 pages
File Size : 54,9 Mb
Release : 1975
Category : Aerodynamics, Supersonic
ISBN : UIUC:30112106612770
Design of a Very-low-bleed Mach 2.5 Mixed-compression Inlet with 45 Percent Internal Contraction by Joseph F. Wasserbauer Pdf
Boundary-layer bleed system study for a full-scale, mixed-compression inlet with 45 percent internal contraction
Author : Robert Joseph Shaw,Joseph F. Wasserbauer,Harvey E. Neumann
Publisher : Unknown
Page : 72 pages
File Size : 51,5 Mb
Release : 1976
Category : Airplanes
ISBN : UIUC:30112105150707
Boundary-layer bleed system study for a full-scale, mixed-compression inlet with 45 percent internal contraction by Robert Joseph Shaw,Joseph F. Wasserbauer,Harvey E. Neumann Pdf
The results of an experimental bleed development study for a full-scale, Mach 2.5, axisymmetric, mixed-compression inlet were presented. The inlet was designed to satisfy the airflow requirements of the TF30-P-3 turbofan engine. Capabilities for porous bleed on the cowl surface and ram-scoop flush-slot bleed on the centerbody were provided. A configuration with no bleed on the cowl achieved a minimum stable, diffuser exit, total pressure recovery of 0.894 with a centerbody-bleed mass flow ratio of 0.02. Configurations with cowl bleed had minimum stable recoveries as high as 0.900 but suffered range decrement penalties from the increased bleed mass flow removal. Limited inlet stability and unstart angle-of-attack data are presented.
International Journal of Turbo & Jet-engines
Author : Anonim
Publisher : Unknown
Page : 484 pages
File Size : 48,7 Mb
Release : 1987
Category : Airplanes
ISBN : UVA:X002069654
International Journal of Turbo & Jet-engines by Anonim Pdf
Paper
Author : Anonim
Publisher : Unknown
Page : 720 pages
File Size : 46,8 Mb
Release : 1985
Category : Mechanical engineering
ISBN : UOM:39015009837611
Paper by Anonim Pdf
An Experimental Investigation of Forced Mixing of a Turbulent Boundary Layer in an Annular Diffuser
Author : Robert Joseph Shaw
Publisher : Unknown
Page : 378 pages
File Size : 46,8 Mb
Release : 1981
Category : Diffusers
ISBN : STANFORD:36105030544394
An Experimental Investigation of Forced Mixing of a Turbulent Boundary Layer in an Annular Diffuser by Robert Joseph Shaw Pdf
Functioning of Inorganic/organic Battery Separators in Silver-zinc Cells
Author : Warren H. Philipp
Publisher : Unknown
Page : 678 pages
File Size : 44,9 Mb
Release : 1976
Category : Electric batteries
ISBN : UFL:31262081360504
Functioning of Inorganic/organic Battery Separators in Silver-zinc Cells by Warren H. Philipp Pdf
Distortion in a Full-scale Bicone Inlet with Internal Focused Compression and 45 Percent Internal Contraction
Author : Joseph F. Wasserbauer,Harvey E. Neumann,Robert Joseph Shaw
Publisher : Unknown
Page : 60 pages
File Size : 47,8 Mb
Release : 1974
Category : Air ducts
ISBN : UIUC:30112106612754
Distortion in a Full-scale Bicone Inlet with Internal Focused Compression and 45 Percent Internal Contraction by Joseph F. Wasserbauer,Harvey E. Neumann,Robert Joseph Shaw Pdf
Bibliography on Aerodynamics of Airframe/engine Integration of High-speed Turbine-powered Aircraft
Author : Mark R. Nichols
Publisher : Unknown
Page : 100 pages
File Size : 50,6 Mb
Release : 1980
Category : Aerodynamics
ISBN : UIUC:30112105146044