Survey And Bibliography On Attainment Of Laminar Flow Control In Air Using Pressure Gradient And Suction

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NASA Technical Memorandum

Author : Anonim
Publisher : Unknown
Page : 92 pages
File Size : 53,9 Mb
Release : 1982
Category : Aeronautics
ISBN : MINN:31951000845352D

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NASA Technical Memorandum by Anonim Pdf

NASA Reference Publication

Author : Anonim
Publisher : Unknown
Page : 984 pages
File Size : 53,8 Mb
Release : 1977
Category : Astronautics
ISBN : MINN:31951D00023604W

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NASA Reference Publication by Anonim Pdf

Applied Mechanics Reviews

Author : Anonim
Publisher : Unknown
Page : 932 pages
File Size : 50,8 Mb
Release : 1980
Category : Mechanics, Applied
ISBN : OSU:32435026161000

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Applied Mechanics Reviews by Anonim Pdf

IUTAM Laminar-Turbulent Transition

Author : Spencer Sherwin,Peter Schmid,Xuesong Wu
Publisher : Springer Nature
Page : 809 pages
File Size : 44,7 Mb
Release : 2021-07-30
Category : Computers
ISBN : 9783030679026

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IUTAM Laminar-Turbulent Transition by Spencer Sherwin,Peter Schmid,Xuesong Wu Pdf

This volume comprises the carefully revised papers of the 9th IUTAM Symposium on Laminar-Turbulent Transition, held at the Imperial College, London, UK, in September 2019. The papers focus on the leading research in understanding transition to turbulence, which is a challenging topic of fluid mechanics and arises in many modern technologies as well as in nature. The proceedings are of interest for researchers in fluid mechanics and industry who have to handle these types of problems, such as in the aeronautical sector.

New Results in Numerical and Experimental Fluid Mechanics XII

Author : Andreas Dillmann,Gerd Heller,Ewald Krämer,Claus Wagner,Cameron Tropea,Suad Jakirlić
Publisher : Springer Nature
Page : 867 pages
File Size : 46,5 Mb
Release : 2019-09-26
Category : Technology & Engineering
ISBN : 9783030252533

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New Results in Numerical and Experimental Fluid Mechanics XII by Andreas Dillmann,Gerd Heller,Ewald Krämer,Claus Wagner,Cameron Tropea,Suad Jakirlić Pdf

This book gathers contributions to the 21st biannual symposium of the German Aerospace Aerodynamics Association (STAB) and the German Society for Aeronautics and Astronautics (DGLR). The individual chapters reflect ongoing research conducted by the STAB members in the field of numerical and experimental fluid mechanics and aerodynamics, mainly for (but not limited to) aerospace applications, and cover both nationally and EC-funded projects. Special emphasis is given to collaborative research projects conducted by German scientists and engineers from universities, research-establishments and industries. By addressing a number of cutting-edge applications, together with the relevant physical and mathematics fundamentals, the book provides readers with a comprehensive overview of the current research work in the field. The book’s primary emphasis is on aerodynamic research in aeronautics and astronautics, and in ground transportation and energy as well.

Innovation in Flight

Author : Joseph R. Chambers
Publisher : Unknown
Page : 406 pages
File Size : 52,8 Mb
Release : 2005
Category : Aeronautics
ISBN : IND:30000109243109

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Innovation in Flight by Joseph R. Chambers Pdf

Stability of Time Dependent and Spatially Varying Flows

Author : D.L. Dwoyer,M.Y. Hussaini
Publisher : Springer Science & Business Media
Page : 361 pages
File Size : 48,6 Mb
Release : 2013-03-09
Category : Science
ISBN : 9781461247241

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Stability of Time Dependent and Spatially Varying Flows by D.L. Dwoyer,M.Y. Hussaini Pdf

This volume is the collection of papers presented at the workshop on 'The Stability of Spatially Varying and Time Dependent Flows" sponsored by the Institute for Computer Applications in Science and Engineering (lCASE) and NASA Langley Research Center (LaRC) during August 19- 23, 1985. The purpose of this workshop was to bring together some of the experts in the field for an exchange of ideas to update the current status of knowledge and to help identify trends for future research. Among the invited speakers were D.M. Bushnell, M. Goldstein, P. Hall, Th. Herbert, R.E. Kelly, L. Mack, A.H. Nayfeh, F.T. Smith, and C. von Kerczek. The contributed papers were by A. Bayliss, R. Bodonyi, S. Cowley, C. Grosch, S. Lekoudis, P. Monkewitz, A. Patera, and C. Streett. In the first article, Bushnell provides a historical background on laminar flow control (LFC) research and summarizes the crucial role played by stability theory in LFC system design. He also identifies problem areas in stability theory requiring further research from the view-point of ap plications to LFC design. It is an excellent article for theoreticians looking for some down-to-earth applications of stability theory.

Experimental Investigation of Turbulent Boundary Layer with Uniform Blowing at Moderate and High Reynolds Numbers

Author : Gazi Hasanuzzaman
Publisher : Cuvillier Verlag
Page : 180 pages
File Size : 41,9 Mb
Release : 2022-01-18
Category : Technology & Engineering
ISBN : 9783736965584

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Experimental Investigation of Turbulent Boundary Layer with Uniform Blowing at Moderate and High Reynolds Numbers by Gazi Hasanuzzaman Pdf

Experimental investigation in turbulent boundary layer flows represents one of the canonical geometries of wall bounded shear flows. Utmost relevance of such experiments, however, is applied in the engineering applications in aerospace and marine industries. In particular, continuous effort is being imparted to explore the underlying physics of the flow in order to develop models for numerical tools and to achieve flow control. Flow control experiments have been widely investigated since 1930’s. Several flow control technique has been explored and have shown potential benefit. But the choice of control technique depends largely on the boundary condition and the type of application. Hence, friction drag of subsonic transport aircraft is intended to be reduced within the scope of this Ph. D. topic. Therefore, application of active control method such as microblowing effect in the incompressible, zero pressure gradient turbulent boundary layer was investigated. A series of experiments have been performed in two different wind tunnel facilities. Wind tunnel from Department of Aerodynamics and Fluid Mechanics (LAS) was used for the measurements for moderate Reynolds number range in co-operation with the wind tunnel from Laboratoire de M´ecanique de Feiret Lille for large Reynolds number range. Measurements are conducted with the help of state-of-the-art techniques such as Laser Doppler Anemometry, Particle Image Velocimetry and electronic pressure sensors.