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An Experimental Investigation Of The Flow In An Axisymmetric Internal Compression Inlet For M 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 An Experimental Investigation Of The Flow In An Axisymmetric Internal Compression Inlet For M book. This book definitely worth reading, it is an incredibly well-written.
Author : Earl C. Watson,William P. Peterson
Publisher : Unknown
Page : 62 pages
File Size : 49,9 Mb
Release : 1961
Category : Aerodynamics, Supersonic
ISBN : UIUC:30112106741678
Author : Anonim
Publisher : Unknown
Page : 392 pages
File Size : 46,9 Mb
Release : 1968
Category : Electronic
ISBN : MINN:319510008461576
Author : Defense Documentation Center (U.S.)
Publisher : Unknown
Page : 1746 pages
File Size : 54,8 Mb
Release : 1961-04
Category : Military art and science
ISBN : UTEXAS:059172131213010
Author : United States. National Aeronautics and Space Administration
Publisher : Unknown
Page : 128 pages
File Size : 42,9 Mb
Release : 1960-07
Category : Electronic
ISBN : STANFORD:36105024165701
Author : Anonim
Publisher : Unknown
Page : 450 pages
File Size : 44,6 Mb
Release : 1960
Category : Aeronautics
ISBN : UVA:X004173290
Author : United States. National Aeronautics and Space Administration
Publisher : Unknown
Page : 448 pages
File Size : 49,9 Mb
Release : 1960
Category : Aeronautics
ISBN : UIUC:30112032439504
Author : Norman D. Wong
Publisher : Unknown
Page : 68 pages
File Size : 54,6 Mb
Release : 1971
Category : Jet engines
ISBN : UIUC:30112106747188
A large-scale, variable-geometry inlet model with a design Mach number of 3.0 was tested at Mach numbers from 1.55 to 3.2. Variable features of the inlet for off-design operation are an adjustable-height ramp system and a translating cowl. This report presents experimental results for a diffuser and boundary-layer bleed configuration which was optimized at the design Mach number. Overall performance was high with throat-mounted vortex generators, which were effective in reducing flow distortion in the subsonic diffuser at the higher Mach numbers.
Author : Anonim
Publisher : Unknown
Page : 104 pages
File Size : 45,7 Mb
Release : 1980
Category : Aeronautics
ISBN : MINN:31951000845247A
Author : Warren E. Anderson,Norman D. Wong
Publisher : Unknown
Page : 68 pages
File Size : 48,7 Mb
Release : 1970
Category : Jet engines
ISBN : STANFORD:36105024774346
Author : Anonim
Publisher : Unknown
Page : 1572 pages
File Size : 49,8 Mb
Release : 1992
Category : Aeronautics
ISBN : UIUC:30112078757413
Author : Anonim
Publisher : Unknown
Page : 1878 pages
File Size : 53,7 Mb
Release : 1961
Category : Government publications
ISBN : UCR:31210023919010
Author : Anonim
Publisher : Unknown
Page : 592 pages
File Size : 55,7 Mb
Release : 1985
Category : Aeronautics
ISBN : MINN:31951000586294T
Author : Library of Congress. Science and Technology Division
Publisher : Unknown
Page : 244 pages
File Size : 46,8 Mb
Release : 1962
Category : Aeronautics
ISBN : MINN:31951P01092133O
Author : Anonim
Publisher : Unknown
Page : 34 pages
File Size : 47,7 Mb
Release : 1960
Category : Electronic
ISBN : NASA:31769000459555
Author : Clifford J. Moore,Dennis M. Phillips
Publisher : Unknown
Page : 492 pages
File Size : 45,7 Mb
Release : 1970
Category : Aeronautics
ISBN : UIUC:30112106859363
This report investigates critical reviews of NACA and NASA report literature on light aircraft design, with emphasis on propulsion subsystems, stability, control, propellers, performance, and safety.