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Small Perturbation Theory

William Rees Sears

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Princeton University Press img Link Publisher

Naturwissenschaften, Medizin, Informatik, Technik / Physik, Astronomie

Beschreibung

Part of the Princeton Aeronautical Paperback series designed to bring to students and research engineers outstanding portions of the twelve-volume High Speed Aerodynamics and Jet Propulsion series. These books have been prepared by direct reproduction of the text from the original series and no attempt has been made to provide introductory material or to eliminate cross reference to other portions of the original volumes.

Originally published in 1960.

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.

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Schlagwörter

Incompressible flow, Phase transition, Equations of motion, Conservative vector field, Approximation, Crocco's theorem, Poisson's equation, Spheroid, Real gas, Temperature gradient, Viscosity, Wind tunnel, Abscissa, Convection, Pressure coefficient, Perturbation theory, Stagnation point, Choked flow, Wave equation, Calculation, Isentropic process, Ludwig Prandtl, Cylindrical coordinate system, Bessel function, Jet propulsion, Lorentz transformation, Explicit formula, Initial condition, Linear differential equation, Perturbation theory (quantum mechanics), Coefficient, Continuity equation, Coordinate system, Velocity, Vorticity, Compressibility, Flow conditions, Speed of sound, Equation of state, Principal value, Velocity gradient, Critical Mach number, Quantity, Prediction, Lift coefficient, Stream function, Amplitude, Downwash, Entropy, Partial differential equation, Theory, Boundary value problem, Reynolds number, Mathematical problem, Airfoil, Boundary layer, Stagnation enthalpy, Aerodynamics, Differential equation, Potential theory, Transonic, Ordinate, Supersonic speed, Affine transformation, Mach number, Sine wave, Compressible flow, Cylinder (geometry), Angle of attack, Adiabatic process