Performance Of Vortex Generators In A Mach 2 5 Low Bleed Full Scale 45 Percent Internal Contraction Axisymmetric Inlet

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NASA Technical Memorandum

Author : Anonim
Publisher : Unknown
Page : 882 pages
File Size : 47,5 Mb
Release : 1976
Category : Aeronautics
ISBN : UOM:39015040296553

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NASA Technical Memorandum by Anonim 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

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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.

NASA SP.

Author : Anonim
Publisher : Unknown
Page : 1066 pages
File Size : 40,5 Mb
Release : 1975
Category : Aeronautics
ISBN : MINN:319510005859970

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NASA SP. by Anonim 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

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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.

Paper

Author : Anonim
Publisher : Unknown
Page : 720 pages
File Size : 46,8 Mb
Release : 1985
Category : Mechanical engineering
ISBN : UOM:39015009837611

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Paper by Anonim 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

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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