Experimental And Theoretical Studies Of Axisymmetric Free Jets
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Experimental And Theoretical Studies Of Axisymmetric Free Jets
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Author :
language : en
Publisher:
Release Date : 1959
Experimental And Theoretical Studies Of Axisymmetric Free Jets written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1959 with Aerodynamics categories.
Some experimental and theoretical studies have been made of axisymmetric free jets exhausting from sonic and supersonic nozzles into still air and into supersonic streams with a view toward problems associated with propulsive jets and the investigation of these problems. For jets exhausting into still air, consideration is given to the effects of jet Mach number, nozzle divergence angle, and jet static-pressure ratio upon jet structure, jet wavelength, and the shape and curvature of the jet boundary. Studies of the effects of the ratio of specific heats of the jets are included as are observations pertaining to jet noise and jet simulation. For jets exhausting into supersonic streams, an attempt has been made to present primarily theoretical curves of the type that may be useful in evaluating certain jet interference effects and in formulating experimental studies. The primary variables considered are jet Mach number, free-stream Mach number, jet static-pressure ratio, ratio of specific heats of the jet, nozzle exit angle, and boattail angle. The simulation problem and the case of a hypothetical hypersonic vehicle are examined. A few experimental observations are included.
Experimental And Theoretical Studies Of Axisymmetric Free Jets
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Author :
language : en
Publisher:
Release Date : 1959
Experimental And Theoretical Studies Of Axisymmetric Free Jets written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1959 with Aerodynamics categories.
Some experimental and theoretical studies have been made of axisymmetric free jets exhausting from sonic and supersonic nozzles into still air and into supersonic streams with a view toward problems associated with propulsive jets and the investigation of these problems. For jets exhausting into still air, consideration is given to the effects of jet Mach number, nozzle divergence angle, and jet static-pressure ratio upon jet structure, jet wavelength, and the shape and curvature of the jet boundary. Studies of the effects of the ratio of specific heats of the jets are included as are observations pertaining to jet noise and jet simulation. For jets exhausting into supersonic streams, an attempt has been made to present primarily theoretical curves of the type that may be useful in evaluating certain jet interference effects and in formulating experimental studies. The primary variables considered are jet Mach number, free-stream Mach number, jet static-pressure ratio, ratio of specific heats of the jet, nozzle exit angle, and boattail angle. The simulation problem and the case of a hypothetical hypersonic vehicle are examined. A few experimental observations are included.
Experimental And Theoretical Studies Of Axisymmetric Free Jets
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Author : Eugene S. Love
language : en
Publisher:
Release Date : 1959
Experimental And Theoretical Studies Of Axisymmetric Free Jets written by Eugene S. Love and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1959 with Aerodynamics categories.
Some experimental and theoretical studies have been made of axisymmetric free jets exhausting from sonic and supersonic nozzles into still air and into supersonic streams with a view toward problems associated with propulsive jets and the investigation of these problems. For jets exhausting into still air, consideration is given to the effects of jet Mach number, nozzle divergence angle, and jet static-pressure ratio upon jet structure, jet wavelength, and the shape and curvature of the jet boundary. Studies of the effects of the ratio of specific heats of the jets are included as are observations pertaining to jet noise and jet simulation. For jets exhausting into supersonic streams, an attempt has been made to present primarily theoretical curves of the type that may be useful in evaluating certain jet interference effects and in formulating experimental studies. The primary variables considered are jet Mach number, free-stream Mach number, jet static-pressure ratio, ratio of specific heats of the jet, nozzle exit angle, and boattail angle. The simulation problem and the case of a hypothetical hypersonic vehicle are examined. A few experimental observations are included.
Experimental And Theoretical Studies Of Axisymmetric Free Jets
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Author :
language : en
Publisher:
Release Date : 1961
Experimental And Theoretical Studies Of Axisymmetric Free Jets written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1961 with Jet engines categories.
Some Studies Of Axisymmetric Free Jets Exhausting From Sonic And Supersonic Nozzles Into Still Air And Into Supersonic Streams
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Author : Eugene S. Love
language : en
Publisher:
Release Date : 1955
Some Studies Of Axisymmetric Free Jets Exhausting From Sonic And Supersonic Nozzles Into Still Air And Into Supersonic Streams written by Eugene S. Love and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1955 with Aerodynamics, Supersonic categories.
Some experimental and theoretical studies have been made of axisymmetric free jets exhausting from sonic and supersonic nozzles into still air and into supersonic streams with a view toward current problems associated with propulsive jets and the investigation of these problems.
Experimental Investigation Of An Axisymmetric Fully Developed Laminar Free Jet
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Author : Eugene P. Symons
language : en
Publisher:
Release Date : 1971
Experimental Investigation Of An Axisymmetric Fully Developed Laminar Free Jet written by Eugene P. Symons and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1971 with Laminar flow categories.
An experimental investigation was conducted to determine dynamic characteristics of a circular, fully developed, laminar free jet. Complete velocity profiles are presented at Reynolds numbers of 437 and 1839 at 0, 3, 6, 10, 15, and 25 diameters from the nozzle exit. Centerline velocity decay was obtained over a range of Reynolds numbers from 255 to 1839. Also presented are the angles of spread associated with the diffusion of the jet downstream of the nozzle. Where possible, results are compared with those obtained for laminar jets having an initially flat or uniform velocity profile at the nozzle exit.
Nasa Technical Report
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Author :
language : en
Publisher:
Release Date : 1959
Nasa Technical Report written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1959 with Aerodynamics categories.
Theoretical And Experimental Investigation Of The Isothermal Axisymmetric Turbulent Free Jet
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Author : David A. Bell
language : en
Publisher:
Release Date : 1984
Theoretical And Experimental Investigation Of The Isothermal Axisymmetric Turbulent Free Jet written by David A. Bell and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1984 with Dissertations, Academic categories.
Capture Of An Axisymmetric Free Jet In A Pipe With Application To Power Augmented Ram Wing Theory
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Author : Harvey R. Chaplin
language : en
Publisher:
Release Date : 1979
Capture Of An Axisymmetric Free Jet In A Pipe With Application To Power Augmented Ram Wing Theory written by Harvey R. Chaplin and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1979 with categories.
A theory of the two-dimensional power-augmented-ram wing with turbulent jets was previously validated over a range of experimental conditions which did not include very small ratios of jet nozzle area to capture area. In the present investigation a simple axisymmetric experiment was conducted to evaluate this condition. Results indicate that the original theory should provide useful predictions regardless of nozzle area ratio. (Author).
Proceedings Of The Third Symposium On The Plasma Sheath Plasma Electromagnetics Of Hypersonic Flight Electrical Properties Of Shock Ionized Flow Fields
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Author :
language : en
Publisher:
Release Date : 1967
Proceedings Of The Third Symposium On The Plasma Sheath Plasma Electromagnetics Of Hypersonic Flight Electrical Properties Of Shock Ionized Flow Fields written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1967 with Aerodynamics, Hypersonic categories.
This volume is a collection of the unclassified papers presented at the Third Symposium on the Plasma Sheath-Plasma Electromagnetics of Hypersonic Flight. This symposium consisted of the review of progress in reentry communication studies during the three year period since the prior meeting. The program of this symposium on plasma electromagnetics of hypersonic flight involves a wide range of scientific disciplines, including electromagnetics, aerodynamics, aero-thermochemistry, plasma dynamics, electronics, and high- temperature phenomena. The papers were selected to explore as many of these facets of research, including the results of laboratory, flight, and system tests, as time permitted.