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Book
Development of form-adaptive airfoil profiles for wind turbine application
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ISBN: 3737603758 9783737603751 9783737603744 373760374X Year: 2017 Publisher: Kassel, Germany : Kassel University Press,

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Keywords

Aerofoils. --- Airfoils


Book
AERODYNAMIQUE EXPERIMENTALE.
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Year: 1950 Publisher: Paris: Béranger,

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Book
TRANSONIC AERODYNAMICS
Authors: --- ---
Year: 1968 Publisher: New York: Academic press,

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Book
Théorie et géométrie de l'hélice marine
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ISBN: 2722503514 9782722503519 Year: 1975 Publisher: Paris : École Nationale Supérieure de Techniques Avancées,

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The paths of soaring flight
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ISBN: 9781848160897 1848160895 1860940552 9781860940552 Year: 1999 Publisher: London : Singapore ; River Edge, NJ : Imperial College Press ; Distributed by World Scientific Pub.,

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This book is concerned with the sport of soaring, mainly with the mathematical basis of sailplane design and operation. It does not tell the beginner how to fly, but it will give an experienced pilot some background, with historical notes showing how ideas have evolved and could develop in the future. Some of the material is taken from OSTIV (Organisation Scientifique et Technique Internationale de Vol a Viole) publications and from Technical Soaring, neither of which is readily available to the general public, including papers by the author and others. Extensive references are provided in eac


Book
General theory of high speed aerodynamics
Author:
Year: 1954 Publisher: Princeton (N.J.): Princeton university press,

Wing theory
Author:
ISBN: 1680158996 9781400860777 1400860776 9781680158991 9780691085364 0691085366 0691604215 9780691604213 0691085366 9780691604213 Year: 1990 Publisher: Princeton, New Jersey : Princeton University Press,

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Originator of many of the theories used in modern wing design, Robert T. Jones surveys the aerodynamics of wings from the early theories of lift to modern theoretical developments. This work covers the behavior of wings at both low and high speeds, including the range from very low Reynolds numbers to the determination of minimum drag at supersonic speed. Emphasizing analytical techniques, Wing Theory provides invaluable physical principles and insights for advanced students, professors, and aeronautical engineers, as well as for scientists involved in computational approaches to the subject. This book is based on over forty years of theoretical and practical work performed by the author and other leading researchers in the field of aerodynamics.Originally published in 1990.The Princeton Legacy Library uses the latest print-on-demand technology to again make available previously out-of-print books from the distinguished backlist of Princeton University Press. These editions preserve the original texts of these important books while presenting them in durable paperback and hardcover editions. The goal of the Princeton Legacy Library is to vastly increase access to the rich scholarly heritage found in the thousands of books published by Princeton University Press since its founding in 1905.


Book
Energy resources and conservation related to built environment. Proceedings of the international conference. Miami Beach, december 7-12, 1980. 2 vol. tome 2
Author:
Year: 1980 Publisher: New York, NY : Pergamon,


Book
Asymptotic Approximations for the Sound Generated by Aerofoils in Unsteady Subsonic Flows
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ISBN: 9783319199597 3319199587 9783319199580 3319199595 Year: 2015 Publisher: Cham : Springer International Publishing : Imprint: Springer,

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This thesis investigates the sound generated by solid bodies in steady subsonic flows with unsteady perturbations, as is typically used when determining the noise generated by turbulent interactions. The focus is predominantly on modelling the sound generated by blades within an aircraft engine, and the solutions are presented as asymptotic approximations. Key analytical techniques, such as the Wiener-Hopf method, and the matched asymptotic expansion method are clearly detailed. The results allow for the effect of variations in the steady flow or blade shape on the noise generated to be analysed much faster than when solving the problem numerically or considering it experimentally.

Analysis of Low-Speed Unsteady Airfoil Flows
Authors: --- --- --- ---
ISBN: 1281141380 9786611141387 3540273611 3540229329 Year: 2005 Publisher: Berlin, Heidelberg : Springer Berlin Heidelberg : Imprint: Springer,

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This book provides an introduction to unsteady aerodynamics with emphasis on the analysis and computation of inviscid and viscous two-dimensional flows over airfoils at low speeds. It begins with a discussion of the physics of unsteady flows and an explanation of lift and thrust generation, airfoil flutter, gust response and dynamic stall. This is followed by an exposition of the four major calculation methods in currents use, namely inviscid-panel, boundary-layer, viscous-inviscid interaction and Navier-Stokes methods. Undergraduate and graduate students, teachers, scientists and engineers concerned with aeronautical, hydronautical and mechanical engineering problems will gain understanding of the physics of unsteady low-speed flows and an ability to analyze these flows with modern computational methods.

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