Performance Of A 10 Conical Plug Nozzle With Various Primary Flap And Nacelle Configurations At Mach Numbers From 0 To 1 97

Performance Of A 10 Conical Plug Nozzle With Various Primary Flap And Nacelle Configurations At Mach Numbers From 0 To 1 97 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 Performance Of A 10 Conical Plug Nozzle With Various Primary Flap And Nacelle Configurations At Mach Numbers From 0 To 1 97 book. This book definitely worth reading, it is an incredibly well-written.

NASA Technical Memorandum

Anonim
NASA Technical Memorandum Book PDF

Author : Anonim
Publisher : Unknown
Page : 104 pages
File Size : 44,7 Mb
Release : 1980
Category : Aeronautics
ISBN : MINN:31951000845247A

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NASA Technical Memorandum by Anonim Pdf

NASA Reference Publication

Anonim
NASA Reference Publication Book PDF

Author : Anonim
Publisher : Unknown
Page : 116 pages
File Size : 48,9 Mb
Release : 1977
Category : Astronautics
ISBN : OSU:32435020935268

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NASA Reference Publication by Anonim Pdf

Heat-transfer Characteristics of Partially Film Coded Plug Nozzle on a J-85 Afterburning Turbojet Engine

Stanley M. Nosek,David M. Straight
Heat transfer Characteristics of Partially Film Coded Plug Nozzle on a J 85 Afterburning Turbojet Engine Book PDF

Author : Stanley M. Nosek,David M. Straight
Publisher : Unknown
Page : 29 pages
File Size : 44,7 Mb
Release : 1976
Category : Airplanes
ISBN : STANFORD:36105024824364

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Heat-transfer Characteristics of Partially Film Coded Plug Nozzle on a J-85 Afterburning Turbojet Engine by Stanley M. Nosek,David M. Straight Pdf

Plug nozzle film cooling data were obtained downstream of a slot located at 42 percent of the total plug length on a J-85 engine. Film cooling reduced the aft end wall temperature as much as 150 K, reduced total pressure loss in the upstream convection cooling passages by 50 percent, and reduced estimated compressor bleed flow requirement by 14 percent compared to an all convectively cooled nozzle. Shock waves along the plug surface strongly influenced temperature distributions on both convection and film cooled portions. The effect was most severe at nozzle pressure ratios below 10 where adverse pressure gradients were most severe.

1975 Ride Quality Symposium

Anonim
1975 Ride Quality Symposium Book PDF

Author : Anonim
Publisher : Unknown
Page : 952 pages
File Size : 54,8 Mb
Release : 1975
Category : Vehicles
ISBN : UFL:31262081360595

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1975 Ride Quality Symposium by Anonim Pdf

Thrust Performance of Isolated Plug Nozzles with Two Types of 40-spoke Noise Suppressor at Mach Numbers from 0 to 0.45

Douglas E. Harrington,James J. Schloemar
Thrust Performance of Isolated Plug Nozzles with Two Types of 40 spoke Noise Suppressor at Mach Numbers from 0 to 0 45 Book PDF

Author : Douglas E. Harrington,James J. Schloemar
Publisher : Unknown
Page : 44 pages
File Size : 45,5 Mb
Release : 1974
Category : Airplanes
ISBN : STANFORD:36105024782695

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Thrust Performance of Isolated Plug Nozzles with Two Types of 40-spoke Noise Suppressor at Mach Numbers from 0 to 0.45 by Douglas E. Harrington,James J. Schloemar Pdf

Plug nozzles with two types of 40-spoke noise suppressor were tested at free-stream Mach numbers from 0 to 0.45 and over a range of nozzle pressure ratios from 1.5 to 4.0. In addition, an unsuppressed plug nozzle and a Supersonic Tunnel Association nozzle were also tested to provide baseline levels of thrust performance. The unsuppressed plug nozzle had an efficiency of 98 percent at an assumed takeoff pressure ratio of 3.0 and at Mach 0.36. At the same condition the suppressor nozzles had efficiencies of approximately 83.5 percent.

Thrust performance of isolated two dimension suppressed plug nozzles with and without ejectors at mach numbers from 0 to 0.45

Douglas E. Harrington,James J. Schloemer,Stanley A. Skebe
Thrust performance of isolated two dimension suppressed plug nozzles with and without ejectors at mach numbers from 0 to 0 45 Book PDF

Author : Douglas E. Harrington,James J. Schloemer,Stanley A. Skebe
Publisher : Unknown
Page : 44 pages
File Size : 45,5 Mb
Release : 1976
Category : Airplanes
ISBN : UIUC:30112106612978

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Thrust performance of isolated two dimension suppressed plug nozzles with and without ejectors at mach numbers from 0 to 0.45 by Douglas E. Harrington,James J. Schloemer,Stanley A. Skebe Pdf

Cold-flow Performance of Several Variations of a Ram-air-cooled Plug Nozzle for Supersonic-cruise Aircraft

Douglas E. Harrington,Stanley M. Nosek,David M. Straight
Cold flow Performance of Several Variations of a Ram air cooled Plug Nozzle for Supersonic cruise Aircraft Book PDF

Author : Douglas E. Harrington,Stanley M. Nosek,David M. Straight
Publisher : Unknown
Page : 44 pages
File Size : 43,5 Mb
Release : 1974
Category : Jet nozzles
ISBN : UIUC:30112106661660

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Cold-flow Performance of Several Variations of a Ram-air-cooled Plug Nozzle for Supersonic-cruise Aircraft by Douglas E. Harrington,Stanley M. Nosek,David M. Straight Pdf