Internal Performance Characteristics Of Thrust Vectored Axisymmetric Ejector Nozzles

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Scientific and Technical Aerospace Reports

Author : Anonim
Publisher : Unknown
Page : 376 pages
File Size : 47,9 Mb
Release : 1995
Category : Aeronautics
ISBN : MINN:30000011064601

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Scientific and Technical Aerospace Reports by Anonim Pdf

Lists citations with abstracts for aerospace related reports obtained from world wide sources and announces documents that have recently been entered into the NASA Scientific and Technical Information Database.

NASA Technical Memorandum

Author : Anonim
Publisher : Unknown
Page : 176 pages
File Size : 53,7 Mb
Release : 1996
Category : Aeronautics
ISBN : STANFORD:36105024157922

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NASA Technical Memorandum by Anonim Pdf

Aeronautical Engineering

Author : Anonim
Publisher : Unknown
Page : 538 pages
File Size : 50,7 Mb
Release : 1991
Category : Aeronautics
ISBN : UOM:39015023295143

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Aeronautical Engineering by Anonim Pdf

93-2400 - 93-2447

Author : Anonim
Publisher : Unknown
Page : 664 pages
File Size : 45,5 Mb
Release : 1992
Category : Airplanes
ISBN : PSU:000023301887

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93-2400 - 93-2447 by Anonim Pdf

Initial Flight Test Evaluation of the F-15 ACTIVE Axisymmetric Vectoring Nozzle Performance

Author : John S. Orme
Publisher : Unknown
Page : 26 pages
File Size : 46,8 Mb
Release : 1998
Category : Black Widow (Night fighter plane)
ISBN : NASA:31769000627862

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Initial Flight Test Evaluation of the F-15 ACTIVE Axisymmetric Vectoring Nozzle Performance by John S. Orme Pdf

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.

Research and Technology Highlights, 1993

Author : Anonim
Publisher : Unknown
Page : 272 pages
File Size : 40,8 Mb
Release : 1994
Category : Electronic
ISBN : NASA:31769000523129

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Research and Technology Highlights, 1993 by Anonim Pdf