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Aerodynamics: Fundamentals of Theory, Aerodynamics of an Airfoil and Wing. Methods of Aerodynamic Calculation: N.F. Krasnov

Aerodynamics is the theoretical foundation of aeronautical, rocket, space, and artillery engineering and the cornerstone of the aerodynamic design of modern craft. The fundamentals of aerodynamics are used in studying the external flow over various bodies or the motion of air (a gas) inside various objects. Engineering success in the fields of aviation, artillery, rocketry, space flight, motor vehicle transport, and so on, i.e. fields that pertain to the flow of air or a gas in some form or other, depends on a firm knowledge of aerodynamics. The present textbook, in addition to the general laws of flow of a fluid, treats the application of aerodynamics, chiefly in rocketry and modern hig speed aviation. The book consists of two parts, each forming a separate volume. ?he first of them concerns the fundamental concepts and definitions or' aerodynamics and the theory of flow over an airfoil and a wing, including an unsteady flow (Chapters 1-9), while the second describes the aerodynamic design of craft and their individual parts (Chapters 10-15). The two parts are designed for use in a two-semester course of aerodynamics, although the first part can be used idependently by those interested in individual problems of theoretical aerodynamics.

A sound theoretical background is important to the study of any subject because creative solutions of practical problems, scientific research, and discoveries are impossible without it. Students should therefore devote special attention to the first live chapters, which deal with the fundamental concepts and definitions of aerodynamics, the kinematics of a fluid, the fundamentals of l]uid dynamics, the theory of shocks, and the method of characteristics used widely in investigating supersonic flows. Chapters 6 and 7, which relate to the tlow over airfoils, are also important to a fundamental understaIding of the subject. These chapters contain a fairly complete discussion of the general theory of flow of a gas in two-dimensional space (the theory of two-dimensional flow). The information on the supersonic steady flow over a wing in Chapter 8 relates directly to these materials. The aerodynamic design of most modern craft is based on studies of such flow.

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