Librería: Used Book Company, Egg Harbor Township, NJ, Estados Unidos de America
EUR 6,37
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Añadir al carritopaperback. Condición: Good. Connecting readers with great books since 1972! Used textbooks may not include companion materials such as access codes, etc. May have some wear or writing/highlighting. We ship orders daily and Customer Service is our top priority!
Librería: HPB Inc., Dallas, TX, Estados Unidos de America
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Añadir al carritoPaperback. Condición: Very Good. Connecting readers with great books since 1972! Used books may not include companion materials, and may have some shelf wear or limited writing. We ship orders daily and Customer Service is our top priority!
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Añadir al carritoPaperback. Condición: Very Good. Connecting readers with great books since 1972! Used books may not include companion materials, and may have some shelf wear or limited writing. We ship orders daily and Customer Service is our top priority!
Librería: AVON HILL BOOKS, Cambridge, MA, Estados Unidos de America
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Añadir al carritoSoftcover. Condición: Fine. 8vo 8" - 9" tall; 672 pp; Dover Books On Aeronautical Engineering.
Librería: INDOO, Avenel, NJ, Estados Unidos de America
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Añadir al carritoPaperback. Condición: Brand New. 672 pages. 8.50x6.00x1.50 inches. In Stock.
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Añadir al carritopaperback. Condición: New. In shrink wrap. Looks like an interesting title!
Idioma: Inglés
Publicado por New York, Dover Publications, 1959, 1945, 1959
ISBN 10: 0486605418 ISBN 13: 9780486605418
Librería: Joseph Valles - Books, Stockbridge, GA, Estados Unidos de America
EUR 60,11
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Añadir al carritoAudio Book (CD). Condición: Very Good. 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. Book.