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Static Internal Performance Of An Axisymmetric Nozzle With Multiaxis Thrust Vectoring Capability 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 Static Internal Performance Of An Axisymmetric Nozzle With Multiaxis Thrust Vectoring Capability book. This book definitely worth reading, it is an incredibly well-written.
Author : George T. Carson
Publisher : Unknown
Page : 88 pages
File Size : 42,9 Mb
Release : 1991
Category : Airplanes
ISBN : STANFORD:36105113791946
Author : Francis J. Capone
Publisher : Unknown
Page : 276 pages
File Size : 49,5 Mb
Release : 1993
Category : Electronic
ISBN : NASA:31769000522196
Author : David J. Wing
Publisher : Unknown
Page : 88 pages
File Size : 53,8 Mb
Release : 1992
Category : Airplanes
ISBN : UIUC:30112106673442
Author : George T. Carson (Jr.)
Publisher : Unknown
Page : 84 pages
File Size : 46,5 Mb
Release : 1991
Category : Electronic
ISBN : NASA:31769000520307
Author : David J. Wing
Publisher : Unknown
Page : 132 pages
File Size : 47,6 Mb
Release : 1994
Category : Electronic
ISBN : NASA:31769000447303
Author : George T. Carson
Publisher : Unknown
Page : 84 pages
File Size : 52,8 Mb
Release : 1991
Category : Airplanes
ISBN : UIUC:30112106567230
Author : National Aeronautics and Space Administration (NASA)
Publisher : Createspace Independent Publishing Platform
Page : 52 pages
File Size : 53,8 Mb
Release : 2018-07-16
Category : Electronic
ISBN : 1722772212
An investigation was conducted in the static test facility of the Langley 16-Foot Transonic Tunnel to determine the flow-turning capability and the nozzle internal performance of an axisymmetric convergent-divergent nozzle with post-exit vanes installed for multiaxis thrust vectoring. The effects of vane curvature, vane location relative to the nozzle exit, number of vanes, and vane deflection angle were determined. A comparison of the post-exit-vane thrust-vectoring concept with other thrust-vectoring concepts is provided. All tests were conducted with no external flow, and nozzle pressure ratio was varied from 1.6 to 6.0. Berrier, Bobby L. and Mason, Mary L. Langley Research Center...
Author : Mary L. Mason
Publisher : Unknown
Page : 172 pages
File Size : 40,8 Mb
Release : 1992
Category : Airplanes
ISBN : UIUC:30112005556599
Author : John S. Orme
Publisher : Unknown
Page : 26 pages
File Size : 43,5 Mb
Release : 1998
Category : Black Widow (Night fighter plane)
ISBN : NASA:31769000627862
A full envelope database of a thrust-vectoring axisymmetric nozzle perfomance for the Pratt & Whitney Pitch/Yaw Balance Beam Nozzle (P/YBBN) is being developed using the F-15 Advanced Control Technology for Integrated Vehicles (ACTIVE) aircraft. At this time, flight research has been completed for steady-state pitch vector angles up to 20 deg. at an altitude of 30,000 ft from low power settings to maximum afterburner power. The nozzle performance database includes vector forces, internal nozzle pressures, and temperatures all of which can be used for regression analysis modeling. The database was used to substantiate a set of nozzle performance data from wind tunnel testing and computational fluid dynamic analyses. Findings from initial flight research at Mach 0.9 and 1.2 are presented in this paper. The results show that vector efficiency is strongly influenced by power setting. A significant discrepancy in nozzle performance has been discovered between predicted and measured results during vectoring.
Author : Anonim
Publisher : Unknown
Page : 90 pages
File Size : 54,7 Mb
Release : 1992
Category : Science
ISBN : STANFORD:36105024801313
Author : Anonim
Publisher : Unknown
Page : 180 pages
File Size : 50,5 Mb
Release : 1987
Category : Aeronautics
ISBN : UIUC:30112104414666
Author : Scott C. Asbury
Publisher : Unknown
Page : 142 pages
File Size : 52,6 Mb
Release : 1999
Category : Boundary layer
ISBN : NASA:31769000633902
Author : United States. National Aeronautics and Space Administration
Publisher : Unknown
Page : 432 pages
File Size : 43,5 Mb
Release : 1990
Category : Aeronautics
ISBN : UOM:39015022363397
Author : Anonim
Publisher : Unknown
Page : 180 pages
File Size : 44,7 Mb
Release : 1992
Category : Aeronautics
ISBN : MINN:31951P00297769K
Author : Bobby L. Berrier
Publisher : Unknown
Page : 62 pages
File Size : 41,7 Mb
Release : 1988
Category : Airplanes
ISBN : NASA:31769000441900