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Theoretical And Experimental Investigation Of The Isothermal Axisymmetric Turbulent Free Jet
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Book Synopsis Theoretical and Experimental Investigation of the Isothermal Axisymmetric Turbulent Free Jet by : David A. Bell
Download or read book Theoretical and Experimental Investigation of the Isothermal Axisymmetric Turbulent Free Jet written by David A. Bell and published by . This book was released on 1984 with total page 206 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Experimental Investigation of an Axisymmetric Fully Developed Laminar Free Jet by : Eugene P. Symons
Download or read book Experimental Investigation of an Axisymmetric Fully Developed Laminar Free Jet written by Eugene P. Symons and published by . This book was released on 1971 with total page 28 pages. Available in PDF, EPUB and Kindle. Book excerpt: 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.
Book Synopsis Experimental Investigation of Organized Structures in the Development Region of an Axisymmetric Turbulent Jet by : Larry P. Marini
Download or read book Experimental Investigation of Organized Structures in the Development Region of an Axisymmetric Turbulent Jet written by Larry P. Marini and published by . This book was released on 1987 with total page 92 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis A Theoretical and Experimental Investigation of Turbulent Jet Interaction by : Steven Brian Weeks
Download or read book A Theoretical and Experimental Investigation of Turbulent Jet Interaction written by Steven Brian Weeks and published by . This book was released on 1969 with total page 96 pages. Available in PDF, EPUB and Kindle. Book excerpt: The interaction of two impinging plane turbulent jets was investigated for the purpose of understanding the performance of proportional fluid amplifiers and momentum-exchange devices. Velocity and turbulence profiles were measured across and at various distances along the combined jet axis through the use of a constant temperature hot-wire anemometer. Experimentally determined jet deflection angles were found to agree with those predicted in a previous work by the free-streamline theory. The results, which are presented in terms of normalized parameters, show that the jet interaction may be divided into three regions: mixing; transition; and fully developed. A vena-contracta effect was found to exist in the mixing region. A discussion of each of the three regions is presented in detail along with generalizations for similar geometries. (Author).
Book Synopsis An Experimental Investigation of a Non-isothermal Turbulent Wall Jet by : Jack Duane Wilson
Download or read book An Experimental Investigation of a Non-isothermal Turbulent Wall Jet written by Jack Duane Wilson and published by . This book was released on 1968 with total page 320 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Experimental Investigation of the Turbulent Axisymmetric Jet by : Steven P. Capp
Download or read book Experimental Investigation of the Turbulent Axisymmetric Jet written by Steven P. Capp and published by . This book was released on 1983 with total page 376 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Experimental and Theoretical Studies of Axisymmetric Free Jets by :
Download or read book Experimental and Theoretical Studies of Axisymmetric Free Jets written by and published by . This book was released on 1959 with total page 300 pages. Available in PDF, EPUB and Kindle. Book excerpt: 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.
Book Synopsis An Experimental Investigation of Three-dimensional Free Mixing of Incompressible, Turbulent, Free Jets by : Nicholas Trentacoste
Download or read book An Experimental Investigation of Three-dimensional Free Mixing of Incompressible, Turbulent, Free Jets written by Nicholas Trentacoste and published by . This book was released on 1966 with total page 72 pages. Available in PDF, EPUB and Kindle. Book excerpt: An experimental investigation of the bulk properties of turbulent, three-dimensional, incompressible, air jets issuing into a quiescent air ambient is presented. The jet orifices utilized included rectangular, elliptical, axisymmetric and triangular geometries. Experimental results of pertinent mean flow properties such as axis velocity decay, half-width growth, etc., are reported. The flow fields of such jets are found to be characterized by three distinct regions in the axis velocity decay. The results obtained lead to the conclusion that low-speed jets which originate from non-axisymmetric orifices decay to axisymmetry far downstream of the jet exit. (Author).
Book Synopsis Turbulent Heat and Mass Transfer in Axisymmetric Jets by : Robert Francis Mons
Download or read book Turbulent Heat and Mass Transfer in Axisymmetric Jets written by Robert Francis Mons and published by . This book was released on 1971 with total page 137 pages. Available in PDF, EPUB and Kindle. Book excerpt: The problem of turbulent mixing is examined with emphasis on mass, momentum, and energy transport in an axisymmetric free jet. An experimental investigation of the response of a pitot tube, a thermocouple and a sampling probe to a known periodic fluctuating flow with variable intensity of fluctuations is performed. The results indicate that the pitot tube response yields an adequate measure of the mean momentum flux in the incompressible range for any level of velocity fluctuation intensity in the direction of the probe axis. On the other hand, the thermocouple and sampling probe are found to be subject to significant errors in the measurement of mean temperature and mean concentration, respectively, in the high shear regions of a turbulent free jet. An experimental examination of the flow field of a turbulent axisymmetric free jet for non-homogeneous and non-isothermal conditions is performed. New probes are developed specifically for measuring these flux quantities. (Author).
Book Synopsis An Experimental Investigation of the Effects of Transverse Secondary Flow on the Laminar-turbulent Transition of a Free Axisymmetric Jet by : Michael Arthur Boyd
Download or read book An Experimental Investigation of the Effects of Transverse Secondary Flow on the Laminar-turbulent Transition of a Free Axisymmetric Jet written by Michael Arthur Boyd and published by . This book was released on 1965 with total page 264 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Experimental Investigation of an Axisymmetric Fully Developed Laminar Free Jet by : Eugene P. Symons
Download or read book Experimental Investigation of an Axisymmetric Fully Developed Laminar Free Jet written by Eugene P. Symons and published by . This book was released on 1971 with total page 18 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Theoretical and experimental investigation of three dimensional turbulent missing in jets and ducts by : George Willis Carroll
Download or read book Theoretical and experimental investigation of three dimensional turbulent missing in jets and ducts written by George Willis Carroll and published by . This book was released on 1980 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Conger Family Bible Records written by and published by . This book was released on with total page 3 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Free Turbulent Mixing by : Philip Thomas Harsha
Download or read book Free Turbulent Mixing written by Philip Thomas Harsha and published by . This book was released on 1971 with total page 340 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Experimental Investigation of Submerged, Turbulent, Axisymmetric Air Jet Impinging on a Flat Plate by : Lan Xiao
Download or read book Experimental Investigation of Submerged, Turbulent, Axisymmetric Air Jet Impinging on a Flat Plate written by Lan Xiao and published by . This book was released on 1993 with total page 216 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Experimental and Theoretical Studies of Axisymmetric Free Jets by :
Download or read book Experimental and Theoretical Studies of Axisymmetric Free Jets written by and published by . This book was released on 1959 with total page 292 pages. Available in PDF, EPUB and Kindle. Book excerpt: 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.
Book Synopsis Experimental and Theoretical Studies of Axisymmetric Free Jets by : Eugene S. Love
Download or read book Experimental and Theoretical Studies of Axisymmetric Free Jets written by Eugene S. Love and published by . This book was released on 1959 with total page 292 pages. Available in PDF, EPUB and Kindle. Book excerpt: 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.
