Author : George T. Carson
Publisher : Unknown
Page : 132 pages
File Size : 49,5 Mb
Release : 1984
Category : Jet nozzles
ISBN : UIUC:30112106715466
Aeropropulsive Characteristics Of Nonaxisymmetric Nozzle Thrust Reversers At Mach Numbers From 0 To 1 20
Aeropropulsive Characteristics Of Nonaxisymmetric Nozzle Thrust Reversers At Mach Numbers From 0 To 1 20 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 Aeropropulsive Characteristics Of Nonaxisymmetric Nozzle Thrust Reversers At Mach Numbers From 0 To 1 20 book. This book definitely worth reading, it is an incredibly well-written.
Aeropropulsive Characteristics of Nonaxisymmetric-nozzle Thrust Reversers at Mach Numbers from 0 to 1.20
Author : Anonim
Publisher : Unknown
Page : 132 pages
File Size : 51,6 Mb
Release : 1984
Category : Electronic
ISBN : NASA:31769000437346
Aeropropulsive Characteristics of Nonaxisymmetric-nozzle Thrust Reversers at Mach Numbers from 0 to 1.20 by Anonim Pdf
NASA Scientific and Technical Publications
Author : Anonim
Publisher : Unknown
Page : 62 pages
File Size : 50,6 Mb
Release : 1989
Category : Aeronautics
ISBN : STANFORD:36105024715968
NASA Scientific and Technical Publications by Anonim Pdf
Scientific and Technical Aerospace Reports
Author : Anonim
Publisher : Unknown
Page : 956 pages
File Size : 41,5 Mb
Release : 1987
Category : Aeronautics
ISBN : UIUC:30112075701463
Scientific and Technical Aerospace Reports by Anonim Pdf
Aeropulsive Characteristics at Mach Numbers Up to 2.2 of Axisymmetric and Nonaxisymmetric Nozzles Installed on an F-18 Model
Author : Francis J. Capone
Publisher : Unknown
Page : 84 pages
File Size : 41,6 Mb
Release : 1982
Category : Jet nozzles
ISBN : UIUC:30112101593462
Aeropulsive Characteristics at Mach Numbers Up to 2.2 of Axisymmetric and Nonaxisymmetric Nozzles Installed on an F-18 Model by Francis J. Capone Pdf
An investigation to determine the aeropropulsive characteristics of nonaxisymmetric nozzles on an F-18 jet effects model was conducted in the Langley 16-foot transonic tunnel and the AEDC 16-foot supersonic wind tunnel. The performance of a two dimensional convergent-divergent nozzle, a single expansion ramp nozzle, and a wedge nozzle was compared with that of the baseline axisymmetric nozzle. Test data were obtained at static conditions and at Mach numbers from 0.60 to 2.20 at an angle of attack of 0 deg. Nozzle pressure ratio was varied from jet-off to about 20.
NASA Technical Paper
Author : Anonim
Publisher : Unknown
Page : 306 pages
File Size : 46,5 Mb
Release : 1989
Category : Astronautics
ISBN : MINN:31951P000544142
NASA Technical Paper by Anonim Pdf
NASA SP.
Author : Anonim
Publisher : Unknown
Page : 396 pages
File Size : 52,5 Mb
Release : 1962
Category : Aeronautics
ISBN : UOM:39015040281498
NASA SP. by Anonim Pdf
Monthly Catalog of United States Government Publications
Author : United States. Superintendent of Documents
Publisher : Unknown
Page : 128 pages
File Size : 55,5 Mb
Release : 1985
Category : Government publications
ISBN : WISC:89013738190
Monthly Catalog of United States Government Publications by United States. Superintendent of Documents Pdf
February issue includes Appendix entitled Directory of United States Government periodicals and subscription publications; September issue includes List of depository libraries; June and December issues include semiannual index
NASA Scientific and Technical Publications
Author : Anonim
Publisher : Unknown
Page : 396 pages
File Size : 48,6 Mb
Release : 1987
Category : Aeronautics
ISBN : UIUC:30112104414658
NASA Scientific and Technical Publications by Anonim Pdf
Effects of Empennage Surface Location on Aerodynamic Characteristics of a Twin-engine Afterbody Model with Nonaxisymmetric Nozzles
Author : Anonim
Publisher : Unknown
Page : 84 pages
File Size : 53,6 Mb
Release : 1985
Category : Electronic
ISBN : NASA:31769000438195
Effects of Empennage Surface Location on Aerodynamic Characteristics of a Twin-engine Afterbody Model with Nonaxisymmetric Nozzles by Anonim Pdf
Aeropropulsive Characteristics of Isolated Combined Turbojet/ramjet Nozzles at Mach Numbers from 0 to 1.20
Author : Anonim
Publisher : Unknown
Page : 212 pages
File Size : 41,7 Mb
Release : 1988
Category : Electronic
ISBN : NASA:31769000442049
Aeropropulsive Characteristics of Isolated Combined Turbojet/ramjet Nozzles at Mach Numbers from 0 to 1.20 by Anonim Pdf
Aeropropulsive Characteristics of Isolated Combined Turbojet/ramjet Nozzles at Mach Numbers from 0 to 1.20
Author : George T. Carson
Publisher : Unknown
Page : 180 pages
File Size : 42,8 Mb
Release : 1988
Category : Jet nozzles
ISBN : UIUC:30112106606319
Aeropropulsive Characteristics of Isolated Combined Turbojet/ramjet Nozzles at Mach Numbers from 0 to 1.20 by George T. Carson Pdf
Effect of a Trade Between Boattail Angle and Wedge Size on the Performance of a Nonaxisymmetric Wedge Nozzle
Author : George T. Carson
Publisher : Unknown
Page : 72 pages
File Size : 41,6 Mb
Release : 1987
Category : Aerodynamic load
ISBN : UIUC:30112106605766
Effect of a Trade Between Boattail Angle and Wedge Size on the Performance of a Nonaxisymmetric Wedge Nozzle by George T. Carson Pdf
Effect of a Trade Between Boattail Angle and Wedge Size on the Performance of a Nonaxisymmetric Wedge Nozzle
Author : Anonim
Publisher : Unknown
Page : 72 pages
File Size : 48,8 Mb
Release : 1987
Category : Electronic
ISBN : NASA:31769000441124
Effect of a Trade Between Boattail Angle and Wedge Size on the Performance of a Nonaxisymmetric Wedge Nozzle by Anonim Pdf
Interference Effects of Thrust Reversing on Horizontal Tail Effectiveness of Twin-engine Fighter Aircraft at Mach Numbers from 0.15 to 0.90
Author : Anonim
Publisher : Unknown
Page : 108 pages
File Size : 40,6 Mb
Release : 1984
Category : Electronic
ISBN : NASA:31769000437767