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Titlebook: Instabilities and Turbulence in Engineering Flows; D. E. Ashpis,T. B. Gatski,R. Hirsh Book 1993 Springer Science+Business Media Dordrecht

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书目名称Instabilities and Turbulence in Engineering Flows
编辑D. E. Ashpis,T. B. Gatski,R. Hirsh
视频video
丛书名称Fluid Mechanics and Its Applications
图书封面Titlebook: Instabilities and Turbulence in Engineering Flows;  D. E. Ashpis,T. B. Gatski,R. Hirsh Book 1993 Springer Science+Business Media Dordrecht
描述This book contains contributions by colleagues, former students and friends of Professor Eli Reshotko in celebration of his 60th birth­ day. Since Professor Reshotko‘s scientific and engineering contribu­ tions have been in the areas of hydrodynamic stability, transition to turbulence, and boundary layer flows, it is only appropriate that the articles in this volume be devoted to these and related topics. The first two sections focus on instabilities and transition in sub­ sonic and supersonic flows, respectively. The third section deals with developing turbulence, while the the final section treats related prob­ lems in engineering fluid mechanics. The diversity and scope of the articles contained herein exemplify the insight and expertise required in the study of transitional and turbulent flows today - traits which also exemplify Eli Reshotko‘s contributions to these fields. A few of the articles in this volume were presented at a sym­ posium in honor of Eli Reshotko‘s 60th birthday, held in Newport News, Virginia, on July 28, 1991. The symposium was sponsored by lCASE, and organized by M.Y. Hussaini (lCASE) and R. Hirsh (U.S. National Science Foundation). Of those who could not
出版日期Book 1993
关键词flows; fluid mechanics; mechanics; stability; turbulence; turbulent flow
版次1
doihttps://doi.org/10.1007/978-94-011-1743-2
isbn_softcover978-94-010-4764-7
isbn_ebook978-94-011-1743-2Series ISSN 0926-5112 Series E-ISSN 2215-0056
issn_series 0926-5112
copyrightSpringer Science+Business Media Dordrecht 1993
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Observations in Using Linear Stability Theory for 3-D Supersonic Boundary Layersw parameter that appears to correlate for adiabatic-wall boundary-layer flow on rotating cones at low supersonic Mach numbers has been found. Also, an increase of stagnation temperature is found to be only slightly stabilizing.
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The Turbulence Structure in an Eight-Degree Conical Diffuserhe mean velocity profiles is currently being studied. Second, an existing low Reynolds number . - ε closure is being modified to predict this flow. It is expected that the modified closure can be used for similar decreasing adverse pressure gradient flows.
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The Generation of Disturbances in a Boundary Layer by Wall Perturbations: The Vibrating Ribbon Revis source. The resultant flow disturbance is described by the convolution of these two components. Numerical integrations of the Orr-Sommerfeld equation have been obtained for a vibrating ribbon acting on a “parallel” boundary layer.
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Dynamic Modelling of Axial Flow Compression Systemsthis is shown in a plot of Greitzer’s . parameter vs. throttle setting, which compares well with the corresponding map produced experimentally, suggesting that the model will be a useful tool for predicting compressor response.
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