Low Reynolds Number Aerodynamics [electronic resource] : Proceedings of the Conference Notre Dame, Indiana, USA, 5–7 June 1989 /

Current interest in a variety of low Reynolds number applications has focused attention on the design and evaluation of efficient airfoil sections at chord Reynolds numbers from about 100,000 to about 1,000,000. These applications include remotely piloted vehicles (RPVs) at high altitudes, sailplanes, ultra-light man-carrying/man powered aircraft, mini-RPVs at low altitudes and wind turbines/propellers. The purpose of this conference was to bring together those researchers who have been active in areas closely related to this subject. All of the papers presented are research type papers. Main topics are: Airfoil Design and Analysis, Computational Studies, Stability and Transition, Laminar Separation Bubble, Steady and Unsteady Wind Tunnel Experiments and Flight Experiments.

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Bibliographic Details
Main Authors: Mueller, Thomas J. editor., SpringerLink (Online service)
Format: Texto biblioteca
Language:eng
Published: Berlin, Heidelberg : Springer Berlin Heidelberg, 1989
Subjects:Physics., Mechanics., Fluids., Engineering., Applied mathematics., Engineering mathematics., Automotive engineering., Fluid- and Aerodynamics., Appl.Mathematics/Computational Methods of Engineering., Engineering, general., Automotive Engineering.,
Online Access:http://dx.doi.org/10.1007/978-3-642-84010-4
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