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An Evaluation of Jet Simulation Parameters for Nozzle Afterbody Testing at Transonic Mach Numbers

William Lee Peters
4.9/5 (9214 ratings)
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Description:The objective of this investigation was to evaluate various jet simulation parameters in an attempt to establish a method of matching hot jet interference with cold jet flows. Successful parameters were determined based on their ability to correlate integrated afterbody pressure drag, a measurement of aerodynamic interference, for jet flows of varying total temperature. Data used in this investigation were obtained from experiments conducted in the AEDC Propulsion Wind Tunnel (16T) with three different isolated nozzle/afterbody configurations at free-stream Mach numbers from 0.6 to 1.5. Gas temperature effects on pressure drag were acquired with a convergent nozzle utilizing an air/ethylene burner to produce gas temperatures from 540 to 3,300 R. In addition, the jet effects of varying internal nozzle geometry, specifically nozzle divergence half-angle and nozzle exit-to-throat area ratio, were investigated utilizing high-pressure air as the nozzle exhaust gas. Jet simulation parameters were evaluated for jet flows where nozzle exit-to-throat area ratio was varied from 1.0 to approximately 1.5 and where divergence half-angle was varied from 0 to 10 deg.We have made it easy for you to find a PDF Ebooks without any digging. And by having access to our ebooks online or by storing it on your computer, you have convenient answers with An Evaluation of Jet Simulation Parameters for Nozzle Afterbody Testing at Transonic Mach Numbers. To get started finding An Evaluation of Jet Simulation Parameters for Nozzle Afterbody Testing at Transonic Mach Numbers, you are right to find our website which has a comprehensive collection of manuals listed.
Our library is the biggest of these that have literally hundreds of thousands of different products represented.
Pages
102
Format
PDF, EPUB & Kindle Edition
Publisher
—
Release
1976
ISBN
qa8PUniacAwC

An Evaluation of Jet Simulation Parameters for Nozzle Afterbody Testing at Transonic Mach Numbers

William Lee Peters
4.4/5 (1290744 ratings)
Read Now Download now ⏭ listen AudioBook
Description: The objective of this investigation was to evaluate various jet simulation parameters in an attempt to establish a method of matching hot jet interference with cold jet flows. Successful parameters were determined based on their ability to correlate integrated afterbody pressure drag, a measurement of aerodynamic interference, for jet flows of varying total temperature. Data used in this investigation were obtained from experiments conducted in the AEDC Propulsion Wind Tunnel (16T) with three different isolated nozzle/afterbody configurations at free-stream Mach numbers from 0.6 to 1.5. Gas temperature effects on pressure drag were acquired with a convergent nozzle utilizing an air/ethylene burner to produce gas temperatures from 540 to 3,300 R. In addition, the jet effects of varying internal nozzle geometry, specifically nozzle divergence half-angle and nozzle exit-to-throat area ratio, were investigated utilizing high-pressure air as the nozzle exhaust gas. Jet simulation parameters were evaluated for jet flows where nozzle exit-to-throat area ratio was varied from 1.0 to approximately 1.5 and where divergence half-angle was varied from 0 to 10 deg.We have made it easy for you to find a PDF Ebooks without any digging. And by having access to our ebooks online or by storing it on your computer, you have convenient answers with An Evaluation of Jet Simulation Parameters for Nozzle Afterbody Testing at Transonic Mach Numbers. To get started finding An Evaluation of Jet Simulation Parameters for Nozzle Afterbody Testing at Transonic Mach Numbers, you are right to find our website which has a comprehensive collection of manuals listed.
Our library is the biggest of these that have literally hundreds of thousands of different products represented.
Pages
102
Format
PDF, EPUB & Kindle Edition
Publisher
—
Release
1976
ISBN
qa8PUniacAwC

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