Theory of flight - Von Mises, Richard, 1883-1953 (New York : Dover Publications, 1959)
Part One. Equilibrium and steady flow in the atmosphere: Chapter I. The atmosphere at rest. -- Chapter II. Bernoulli´s equation. Influence of humidity. Chapter III. Momentum and energy equations. -- Chapter IV. Perfect and viscous fluids. Types of flow. -- Chapter V. Air resistance, or parasite drag. -- Part Two: The airplane wing. Chapter VI. Fundamental notions. Geometry of wings. -- Chapter VII. Empirical airfoil data. -- Chapter VIII. The wing of infinite span. -- Chapter IX. The wing of finite span. - Chapter X. Additional facts about wings. -- Part Three: Propeller and engine. -- Chapter XI. -- The propeller. -- Chapter XII. -- Outline of propeller theory. -- Chapter XIII. -- The airplane engine. -- Part Four. Airplane performance: Chapter XIV. -- The general performance problem. -- Chapter XV. -- Analytic methods of performance computation. -- Chapter XVI. -- Special performance problems. -- Part Five. Airplane control and stability. -- Chapter XVII. Moment equilibrium and static stability. -- Chapter XVIII. nonuniform flight. -- Chapter XIX. General theory of motion and stability. -- Chapter XX. Dynamic stability of an airplane.
MU
Keywords: Aerodinámica; Motores de aviones