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Theory of flight.

Von Mises, Richard, 1883-1953.

18 valoraciones por Goodreads
ISBN 10: 0486605418 / ISBN 13: 9780486605418
Editorial: New York, Dover Publications, 1959, 1945, 1959
Usado Condición: Very Good Encuadernación de tapa blanda
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Librería en AbeBooks desde: 17 de agosto de 1998

Descripción

629 p. illus. 22 cm. ; ISBN: 0486605418 (pbk.); 9780486605418 LCCN: 59-4203 ; "Unabridged and unaltered republication of the English translation first published . in 1945." ; "Perhaps the most balanced, well-written account of fundamental fluid dynamics ever published. Mises' classic avoids the formidable mathematical structure of fluid dynamics, while conveying - by often unorthodox methods - a full understanding of the physical phenomena and mathematical concepts of aeronautical engineering." ; "An outstanding textbook." - Scientific, Medical and Technical Books. ; green and white paper wrappers ; foxing ; Contents: Equilibrium and steady flow in the atmosphere -- Equilibrium of a Perfect Gas under the Influence of Gravity -- The Standard Atmosphere -- Determination of True Altitude Reduction of a Climb to Standard -- Atmosphere -- Bernoulli's equation -- Dynamic Pressure -- Pressure Distribution -- Influence of Compressibility -- Propeller and engine -- Geometry of Propellers -- Propeller Characteristics -- Quantitative Analysis -- Propeller Sets and Variablepitch Propeller Propeller Chart -- Outline of propeller theory -- Variation of Total Head across the Streamlines Rotation -- Circulation and Rotation -- The Bicirculating Motion -- Flux of Momentum in Steady Flow -- Momentum Equation for Steady Flow -- Moment of Momentum -- Quasisteady Flow Relative Flow -- Energy Equation -- Viscosity -- Law of Similitude Reynolds Number -- Laminar and Turbulent Motion -- Continuous and Discontinuous Motion -- Air resistance or parasite drag -- Bluff Bodies -- Round Bodies -- Streamlined Bodies -- Skin Friction -- Parasite Drag of Major Airplane Components -- The airplane wing -- Geometry of Airfoil Profiles Sets of Profiles -- Theoretically Developed Airfoil Sections -- Geometry of Airplane Wings -- The Three Main Results -- Influence of Aspect Ratio -- Historcal Development of Wing Pro1iles -- Influence of the Shape of tin Profile -- Influence of the Reynolds Number Degree of Turbulence -- The Momentum Equation for Irrotational Wow -- The Lift on an Airfoil of Infinite Span -- The Pitching Moment of an Airfoil of Infinite Span -- The Metacentric Parabola -- Vortex Sheets Another Approach -- Theory of Thin Airfoils -- Curved Vortex Lines -- Vortex Sheet and Discontinuity Surface -- The Flow Past a Wing of Finite Span -- Prandtls Wing Theory -- Ellipiic Lift Distribution -- Biplane Theory -- General Lift Distribution -- Stalling -- Highlift Devices -- Momentum Theory Basic Relations -- Momentum Theory Conclusions -- Modified Momentum Theory -- The Two Theories Combined -- Additional Remarks -- The Engine at Sea Level -- The Engine at Altitude -- Engine Vibrations -- Airplane performance -- Power required and Power available Curves -- Dimensionless Performance Analysis -- Discussion of Sealevel Flight -- Altitude Flight -- Analytical methods of performance computation -- Analytic Expressions for the Power Curves -- Gliding Level Flight with Given Power -- Power Available Independent of Speed -- Numerical Data Example -- Small Variations Choice of Propeller -- Power Available Varying with Speed -- Numerical Discussion -- Special performance problems -- Range and Endurance -- Takeoff -- Steep Gliding and Diving -- Landing Operation Landing Impact -- Seaplane Problems -- Airplane control and stability -- Moment equilibrium and static stability -- Pitching moment Equilibrium -- The Contribution to the Pitching Moment from the Tail -- The Contribution from the Propeller and the Fuselage -- Static Stability and Metaeenter -- Simplified Stability Discussion -- Lateral Moments -- The General Equations of Motion of an Airplane -- Steady Motion Specification of Forces -- Application to the Airplane -- Longitudinal Stability of Level Flight -- The Small Oscillations Following a Disturbance -- Lateral Stability -- Final Remarks -- Autorotation Spinning ; VG. N° de ref. de la librería 005580

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Detalles bibliográficos

Título: Theory of flight.

Editorial: New York, Dover Publications, 1959, 1945

Año de publicación: 1959

Encuadernación: Audio Book (CD)

Condición del libro: Very Good

Tipo de libro: Book

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Sinopsis:

"An outstanding textbook." — Scientific, Medical and Technical Books
Almost unsurpassed as a balanced, well-written account of fundamental fluid dynamics, Theory of Flight may still be recommended for a clearer presentation than is to be forced in many more recent works, though it is limited to situations in which air compressibility effects are unimportant.
Designed for the college senior or beginning graduate student, the text assumes a knowledge of the principles of calculus and some training in general mechanics. It is unusual in offering a well-balanced introduction, stressing equally theory and practice. It avoids the formidable mathematical structure of fluid dynamics, while conveying by often unorthodox methods a full understanding of the physical phenomena and mathematical concepts of aeronautical engineering. Theory of Flight contains perhaps the best introduction to the general theory of stability, while the introduction to dynamics of incompressible fluids and the chapters on wing theory remain particularly valuable for their clarity of exposition and originality of thought.
Mises' position as one of the great pioneers in the development of the aeronautical sciences lends a flavor of authenticity not found in more conventional textbooks. Any student who has made himself familiar with his exposition of the fundamentals and applications will have acquired an excellent background for additional, more specialized fields of modern aeronautical engineering.

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