By John J. Bertin
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Extra resources for Aerodynamics for Engineers,
2 CONSERVATION OF MASS The conservation of mass is one of the most important and useful equations in fluid dynamics. It allows us to determine if a given flow field conserves mass, and is therefore physically possible. If mass is not conserved, then we are wasting our time analyzing the details of the flow, since it cannot occur physically. First, we will apply the principle of conservation of mass to a small volume of space (a control volume) through which the fluid can move freely. It is important to understand that the “walls” of the control volume are fictitious and do not interfere with the flow.
The purpose of the rest of the book is to begin to learn about each of these airplane aerodynamic devices and how they work. 4 SUMMARY Aerodynamics is all about estimating the pressures, shear stresses, heat, lift, drag, and moments created by various airplane components. We do this so that we can estimate the performance and flying characteristics of airplanes, and hopefully design better airplanes than have existed in the past. , viscosity, density, and speed of sound) that have been presented in this chapter.
43 44 Chap. 2 / Fundamentals of Fluid Mechanics The fundamental physical laws used to solve for the fluid motion in a general problem are: 1. Conservation of mass (or the continuity equation) 2. Conservation of linear momentum (or Newton’s second law of motion) 3. Conservation of energy (or the first law of thermodynamics) Because the flow patterns are often very complex, it may be necessary to also use experimental investigations, theoretical analysis, and/or computational simulations to aid in describing the resultant flow.