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book: Wing Theory
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Wing Theory

  • Robert Thomas Jones
Language:English
Published/Copyright:1990
Published by
Princeton University Press
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Princeton Legacy Library
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About this book

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.

ThePrinceton 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.


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Publishing information
Pages and Images/Illustrations in book
eBook published on:
July 14, 2014
eBook ISBN:
9781400860777
Edition:
Course Book
Pages and Images/Illustrations in book
Main content:
228
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eBook ISBN:9781400860777
Keywords for this book
Airfoil;Downwash;Mach number;Angle of attack;Two-dimensional flow;Supersonic speed;Kutta condition;Mach wave;Incompressible flow;Reynolds number;Parasitic drag;Speed of sound;Supercritical airfoil;Trailing edge;Aspect ratio (aeronautics);Lift coefficient;Oblique wing;Calculation;Boundary layer;Area rule;Ellipse;Lift-to-drag ratio;Critical Mach number;Laplace's equation;Vorticity;Potential flow;Plane wave;Horseshoe vortex;Transonic;Two-dimensional space;Dihedral (aeronautics);Cartesian coordinate system;Supersonic wind tunnel;Skin friction drag;Pitching moment;Pressure coefficient;Wind tunnel;Drag coefficient;Navier–Stokes equations;Aerodynamics;Oblique shock;Fineness ratio;Drag polar;Pressure gradient;Choked flow;Viscosity;Canard (aeronautics);Bernoulli's principle;NACA airfoil;Lifting-line theory;Relative velocity;Perfect gas;D'Alembert's paradox;Control volume;Spheroid;Wavefront;Biplane;Velocity;Acceleration;Suction;Constant curvature;Buoyancy;Clark Y;Resultant force;Compressible flow;Right angle;Hyperboloid;C0;Compressibility;Aeromechanics
Audience(s) for this book
College/higher education;Professional and scholarly;
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