Thrust Performance Of Isolated Plug Nozzles With Two Types Of 40 Spoke Noise Suppressor At Mach Numbers From 0 To 0 45

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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

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Author : Douglas E. Harrington
language : en
Publisher:
Release Date : 1974

Thrust Performance Of Isolated Plug Nozzles With Two Types Of 40 Spoke Noise Suppressor At Mach Numbers From 0 To 0 45 written by Douglas E. Harrington and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1974 with Airplanes categories.

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 36 Chute Suppressor Plug Nozzles With And Without Ejectors At Mach Numbers From 0 To 0 45

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Author : Douglas E. Harrington
language : en
Publisher:
Release Date : 1975

Thrust Performance Of Isolated 36 Chute Suppressor Plug Nozzles With And Without Ejectors At Mach Numbers From 0 To 0 45 written by Douglas E. Harrington and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1975 with Airplanes categories.

Exhaust Emissions From A Premixing Prevaporizing Flame Tube Using Liquid Jet A Fuel

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Author : Cecil J. Marek
language : en
Publisher:
Release Date : 1976

Exhaust Emissions From A Premixing Prevaporizing Flame Tube Using Liquid Jet A Fuel written by Cecil J. Marek and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1976 with Aircraft exhaust emissions categories.

The Aeronautical Journal

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Author :
language : en
Publisher:
Release Date : 1974

The Aeronautical Journal written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1974 with Aeronautics categories.

Thrust Performance Of Isolated Two Dimension Suppressed Plug Nozzles With And Without Ejectors At Mach Numbers From 0 To 0 45

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Author : Douglas E. Harrington
language : en
Publisher:
Release Date : 1976

Thrust Performance Of Isolated Two Dimension Suppressed Plug Nozzles With And Without Ejectors At Mach Numbers From 0 To 0 45 written by Douglas E. Harrington and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1976 with Airplanes categories.

Thrust Performance Of Isolated 36 Chute Suppressor Plug Nozzles With And Without Ejectors At Mach Numbers From 0 To 0 45

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Author : Douglas E. Harrington
language : en
Publisher:
Release Date : 1975

Thrust Performance Of Isolated 36 Chute Suppressor Plug Nozzles With And Without Ejectors At Mach Numbers From 0 To 0 45 written by Douglas E. Harrington and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1975 with categories.

Thrust Performance Of Isolated Two Dimensional Suppressed Plug Nozzles With And Without Ejectors At Mach Numbers From 0 To 0 45

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Author : Douglas E. Harrington
language : en
Publisher:
Release Date : 1976

Thrust Performance Of Isolated Two Dimensional Suppressed Plug Nozzles With And Without Ejectors At Mach Numbers From 0 To 0 45 written by Douglas E. Harrington and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1976 with categories.

Off Design Performance Of Two Isentropic Plug Nozzles Designed For A Pressure Ratio Of 16 5

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Author : Bobby L. Berrier
language : en
Publisher:
Release Date : 1967

Off Design Performance Of Two Isentropic Plug Nozzles Designed For A Pressure Ratio Of 16 5 written by Bobby L. Berrier and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1967 with Nozzles categories.

Isolated Performance At Mach Numbers From 0 60 To 2 86 Of Several Expendable Nozzle Concepts For Supersonic Applications

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Author : National Aeronautics and Space Administration (NASA)
language : en
Publisher: Createspace Independent Publishing Platform
Release Date : 2018-06-15

Isolated Performance At Mach Numbers From 0 60 To 2 86 Of Several Expendable Nozzle Concepts For Supersonic Applications written by National Aeronautics and Space Administration (NASA) and has been published by Createspace Independent Publishing Platform this book supported file pdf, txt, epub, kindle and other format this book has been release on 2018-06-15 with categories.

Investigations have been conducted in the Langley 16-Foot Transonic Tunnel (at Mach numbers from 0.60 to 1.25) and in the Langley Unitary Plan Wind Tunnel (at Mach numbers from 2.16 to 2.86) at an angle of attack of 0 deg to determine the isolated performance of several expendable nozzle concepts for supersonic nonaugmented turbojet applications. The effects of centerbody base shape, shroud length, shroud ventilation, cruciform shroud expansion ratio, and cruciform shroud flap vectoring were investigated. The nozzle pressure ratio range, which was a function of Mach number, was between 1.9 and 11.8 in the 16-Foot Transonic Tunnel and between 7.9 and 54.9 in the Unitary Plan Wind Tunnel. Discharge coefficient, thrust-minus-drag, and the forces and moments generated by vectoring the divergent shroud flaps (for Mach numbers of 0.60 to 1.25 only) of a cruciform nozzle configuration were measured. The shortest nozzle had the best thrust-minus-drag performance at Mach numbers up to 0.95 but was approached in performance by other configurations at Mach numbers of 1.15 and 1.25. At Mach numbers above 1.25, the cruciform nozzle configuration having the same expansion ratio (2.64) as the fixed geometry nozzles had the best thrust-minus-drag performance. Ventilation of the fixed geometry divergent shrouds to the nozzle external boattail flow generally improved thrust-minus-drag performance at Mach numbers from 0.60 to 1.25, but decreased performance above a Mach number of 1.25. Re, Richard J. and Berrier, Bobby L. and Abeyounis, William K. Langley Research Center RTOP 706-17-21-05

Performance Of A 10 Deg Conical Plug Nozzle With A Stowed Thrust Reverser At Mach Numbers From 0 To 2 0

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Author : Fred W. Steffen
language : en
Publisher:
Release Date : 1970

Performance Of A 10 Deg Conical Plug Nozzle With A Stowed Thrust Reverser At Mach Numbers From 0 To 2 0 written by Fred W. Steffen and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1970 with categories.