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An Experimental Investigation Of The Effects Of Transverse Secondary Flow On The Laminar Turbulent Transition Of A Free Axisymmetric Jet
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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 Abstracts of Theses and Dissertations by : Auburn University. Graduate School
Download or read book Abstracts of Theses and Dissertations written by Auburn University. Graduate School and published by . This book was released on 1962 with total page 704 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Abstracts of Theses and Titles of Dissertations by : Auburn University. Graduate School
Download or read book Abstracts of Theses and Titles of Dissertations written by Auburn University. Graduate School and published by . This book was released on 1966 with total page 276 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Scientific and Technical Aerospace Reports by :
Download or read book Scientific and Technical Aerospace Reports written by and published by . This book was released on 1992 with total page 316 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis International Aerospace Abstracts by :
Download or read book International Aerospace Abstracts written by and published by . This book was released on 1999 with total page 974 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis An Experimental Investigation of the Effects of a Turbulent Co-flowing Flow on the Development of a Jet by : S. S. I. Rizvi
Download or read book An Experimental Investigation of the Effects of a Turbulent Co-flowing Flow on the Development of a Jet written by S. S. I. Rizvi and published by . This book was released on 1991 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Fluerics by : Diamond (Harry) Laboratories, Washington, D.C.
Download or read book Fluerics written by Diamond (Harry) Laboratories, Washington, D.C. and published by . This book was released on 1970 with total page 384 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author :National Aeronautics and Space Administration (NASA) Publisher :Createspace Independent Publishing Platform ISBN 13 :9781721940462 Total Pages :254 pages Book Rating :4.9/5 (44 download)
Book Synopsis Experimental Investigation of Transition to Turbulence As Affected by Passing Wakes by : National Aeronautics and Space Administration (NASA)
Download or read book Experimental Investigation of Transition to Turbulence As Affected by Passing Wakes written by National Aeronautics and Space Administration (NASA) and published by Createspace Independent Publishing Platform. This book was released on 2018-06-27 with total page 254 pages. Available in PDF, EPUB and Kindle. Book excerpt: Experimental results from a study of the effects of passing wakes upon laminar-to-turbulent transition in a low-pressure turbine passage are presented. The test section geometry is designed to simulate the effects of unsteady wakes resulting from rotor-stator interaction upon laminar-to-turbulent transition in turbine blade boundary layers and separated flow regions over suction surfaces. Single-wire, thermal anemometry techniques were used to measure time-resolved and phase-averaged, wall-normal profiles of velocity, turbulence intensity, and intermittency at multiple streamwise locations over the turbine airfoil suction surface. These data are compared to steady state, wake-free data collected in the same geometry to identify the effects of wakes upon laminar-to-turbulent transition. Results are presented for flows with a Reynolds number based on suction surface length and exit velocity of 50,000 and an approach flow turbulence intensity of 2.5 percent. From these data, the effects of passing wakes and associated increased turbulence levels and varying pressure gradients on transition and separation in the near-wall flow are presented. The results show that the wakes affect transition both by virtue of their difference in turbulence level from that of the free-stream but also by virtue of their velocity deficit relative to the freestream velocity, and the concomitant change in angle of attack and temporal pressure gradients. The results of this study seem to support the theory that bypass transition is a response of the near-wall viscous layer to pressure fluctuations imposed upon it from the free-stream flow. The data also show a significant lag between when the wake is present over the surface and when transition begins. The accompanying CD-ROM includes tabulated data, animations, higher resolution plots, and an electronic copy of this report. Kaszeta, Richard W. and Simon, Terrence W. and Ashpis, David (Technical Monitor) Glenn Research Center NCC3-652; RTOP 71
Book Synopsis Fluid Flow Measurement by : Ruth Rosemary Dowden
Download or read book Fluid Flow Measurement written by Ruth Rosemary Dowden and published by . This book was released on 1972 with total page 258 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Paper written by and published by . This book was released on 1972 with total page 338 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 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:
Download or read book Fluidics Feedback written by and published by . This book was released on 1967 with total page 664 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis An Experimental Study of a Turbulent Axisymmetric Jet Issuing Into a Coflowing Airstream by : S. Biringen
Download or read book An Experimental Study of a Turbulent Axisymmetric Jet Issuing Into a Coflowing Airstream written by S. Biringen and published by . This book was released on 1975 with total page 84 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis An Experimental Investigation of a Turbulent Jet in a Cross Flow by : David Kenneth Mosher
Download or read book An Experimental Investigation of a Turbulent Jet in a Cross Flow written by David Kenneth Mosher and published by . This book was released on 1970 with total page 340 pages. Available in PDF, EPUB and Kindle. Book excerpt: The interference phenomenon occurring when a subsonic turbulent jet exhausts normally from a large flat plate into a low speed crossflow was experimentally investigated in the Georgia Tech nine foot wind tunnel. Static pressures were measured on the surface around the jet. In the region off the surface, including the jet plume, wake and surrounding areas, the average total and static pressures and the average velocity magnitudes and directions were determined. Three jet exit configurations were studied, one circular and two slot-shaped with width to length ratios of 0.3 and 3.4. All have the same exit area. The effective jet to cross-flow velocity ratio was varied, for each of the exit configurations, over the range 4.0 to 12.0. Analysis of the data indicates that the pressure distributions induced on the surface are a combined result of the jet's blocking and entraining effects on the cross flow with entrainment becoming the more dominant of the two as the effective velocity ratio is increased. This relative dominance brings about an attenuation of total interference lift loss (when computed as a fraction of gross thrust) primarily by causing a rise in the low pressures in the wake region as the effective velocity ratio increases. When the effective velocity ratio is held fixed, the total interference lift loss increases with increasing width to length ratio of the jet exit. (Author).
Download or read book Applied Mechanics Reviews written by and published by . This book was released on 1974 with total page 592 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Journal of Dynamic Systems, Measurement, and Control by :
Download or read book Journal of Dynamic Systems, Measurement, and Control written by and published by . This book was released on 1971 with total page 1136 pages. Available in PDF, EPUB and Kindle. Book excerpt:
