Aerodynamics for Engineering StudentsAlready established as the leading course text on aerodynamics, Aerodynamics for Engineering Students has been revised to include the latest developments in flow control and boundary layers, and their influence on modern wing design, as well as introducing recent advances in the understanding of fundamental fluid dynamics. Computational methods have been expanded and updated to reflect the modern approaches to aerodynamic design and research in the aeronautical industry and elsewhere, and the structure of the text has been developed to reflect current course requirements. The book is designed to be accessible and practical. Theory is developed logically within each chapter with notation, symbols and units well defined throughout, and the text is fully illustrated with worked examples and exercises. The classic text, expanded and updated. Includes latest developments in flow control, boundary layers and fluid dynamics. Fully illustrated throughout with illustrations, worked examples and exercises. 
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E L Houghton was one of my lecturers when I was at the Hatfield Polytechnic(now University of Hertfordshire) in the early '80s, so this text book was pretty much mandatory. 25 years on, it is still readable and a good undergraduate text. Recommended
Contents
1  
Chapter 2 Governing equations of fluid mechanics  52 
Chapter 3 Potential flow  104 
Chapter 4 Twodimensional wing theory  159 
Chapter 5 Finite wing theory  210 
Chapter 6 Compressible flow  273 
Chapter 7 Viscous flow and boundary layers  373 
Chapter 8 Flow control and wing design  485 
Chapter 9 Propellers and propulsion  527 
symbols and notation  563 
the international standard atmosphere  567 
a solution of integrals of the type of Glauerts integral  569 
conversion of imperial units to systeme international SI units  572 
574  
577  
Common terms and phrases
adverse pressure gradient aerodynamic aerofoil aerofoil section aircraft airscrew approximation aspect ratio axis body boundary layer calculated camber line chord circular cylinder circulation coefﬁcient compressible computational constant coordinates curve density direction disc distance downstream downwash drag coefficient effect element energy equation expression flat plate flight ﬂow flow field fluid force free stream given gives Gurney flap incompressible increase induced drag integral inviscid laminar leading edge length lift coefficient Mach number mass maximum momentum normal obtained pitching pitching moment plane potential flow pressure distribution radius region result Reynolds number separation shape shear stress shock wave shown in Fig skinfriction drag solution span spanwise speed stagnation point stream function streamlines subsonic tangential theory trailing edge transition turbulent boundary layer unit upper surface variables velocity components velocity potential velocity profile viscous vortex vortices wake wall zero
Popular passages
Page 49  Assuming the period of oscillation of a simple pendulum to depend on the mass of the bob, the length of the pendulum and the acceleration due to gravity g...
Page 10  ... the heat required to increase the temperature of the gas (as in the case at constant volume) and in addition the amount of heat equivalent to the mechanical work done against the force. This total amount of heat is called the 'specific heat at constant pressure', cp, and is defined as 'that amount of heat required to raise the temperature of unit mass of the gas by one degree, the pressure of the gas being kept constant while heating'.
Page 10  The unit for this purpose is the calory or heat unit, being the amount of heat necessary to raise the temperature of unit mass...
Page 22  6' case '7' case '8' case '9' showlmage(' "number ' . Sletter . ""); break; showlmage(' "exclamation mark" ' ); break; #82 Spell Words with Yahoo! Images case ' ?' : showlmage(' "question mark"'); break; case a case 'b...
Page 6  Consequently it may be concluded that the pressure acting at a point in a fluid at rest is the same in all directions.