Author : Milton Lamb
Publisher : Unknown
Page : 232 pages
File Size : 46,9 Mb
Release : 1995
Category : Electronic
ISBN : NASA:31769000523426
Internal Performance Characteristics Of Thrust Vectored Axisymmetric Ejector Nozzles
Internal Performance Characteristics Of Thrust Vectored Axisymmetric Ejector Nozzles 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 Internal Performance Characteristics Of Thrust Vectored Axisymmetric Ejector Nozzles book. This book definitely worth reading, it is an incredibly well-written.
Scientific and Technical Aerospace Reports
Author : Anonim
Publisher : Unknown
Page : 376 pages
File Size : 47,9 Mb
Release : 1995
Category : Aeronautics
ISBN : MINN:30000011064601
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.
Monthly Catalogue, United States Public Documents
Author : Anonim
Publisher : Unknown
Page : 1636 pages
File Size : 42,7 Mb
Release : 1995
Category : Government publications
ISBN : UIUC:30112005602260
Monthly Catalogue, United States Public Documents by Anonim Pdf
Monthly Catalog of United States Government Publications
Author : Anonim
Publisher : Unknown
Page : 1284 pages
File Size : 45,5 Mb
Release : 1994
Category : Government publications
ISBN : WISC:89117117366
Monthly Catalog of United States Government Publications by Anonim Pdf
NASA Technical Memorandum
Author : Anonim
Publisher : Unknown
Page : 176 pages
File Size : 53,7 Mb
Release : 1996
Category : Aeronautics
ISBN : STANFORD:36105024157922
NASA Technical Memorandum by Anonim Pdf
Static Internal Performance Characteristics of Two Thrust-reverser Concepts for Axisymmetric Nozzles
Author : Laurence D. Leavitt,Richard J. Re
Publisher : Unknown
Page : 28 pages
File Size : 52,6 Mb
Release : 1982
Category : Jet planes
ISBN : NASA:31769000434707
Static Internal Performance Characteristics of Two Thrust-reverser Concepts for Axisymmetric Nozzles by Laurence D. Leavitt,Richard J. Re Pdf
Static Internal Performance of an Axisymmetric Nozzle with Multiaxis Thrust-vectoring Capability
Author : George T. Carson
Publisher : Unknown
Page : 0 pages
File Size : 43,9 Mb
Release : 1991
Category : Electronic
ISBN : OCLC:977670793
Static Internal Performance of an Axisymmetric Nozzle with Multiaxis Thrust-vectoring Capability by George T. Carson Pdf
Aeronautical Engineering
Author : Anonim
Publisher : Unknown
Page : 538 pages
File Size : 50,7 Mb
Release : 1991
Category : Aeronautics
ISBN : UOM:39015023295143
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
93-2400 - 93-2447 by Anonim Pdf
33rd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit
Author : Anonim
Publisher : Unknown
Page : 626 pages
File Size : 52,7 Mb
Release : 1997
Category : Airplanes
ISBN : PSU:000032961867
33rd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit 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
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.
30th AIAA/ASME/SAE/ASEE Joint Propulsion Conference
Author : Anonim
Publisher : Unknown
Page : 604 pages
File Size : 42,8 Mb
Release : 1994
Category : Airplanes
ISBN : PSU:000024583442
30th AIAA/ASME/SAE/ASEE Joint Propulsion Conference by Anonim Pdf
Internal Performance of Several Divergent-shroud Ejector Nozzles with High Divergence Angles
Author : Arthur M. Trout,S. Stephen Papell,John H. Povolny
Publisher : Unknown
Page : 70 pages
File Size : 45,7 Mb
Release : 1957
Category : Airplanes
ISBN : UOM:39015086464073
Internal Performance of Several Divergent-shroud Ejector Nozzles with High Divergence Angles by Arthur M. Trout,S. Stephen Papell,John H. Povolny Pdf
Research and Technology Highlights, 1993
Author : Anonim
Publisher : Unknown
Page : 272 pages
File Size : 40,8 Mb
Release : 1994
Category : Electronic
ISBN : NASA:31769000523129
Research and Technology Highlights, 1993 by Anonim Pdf
International Journal of Turbo & Jet-engines
Author : Anonim
Publisher : Unknown
Page : 364 pages
File Size : 54,6 Mb
Release : 1994
Category : Airplanes
ISBN : UVA:X002723339