000			02840cam a2200253 a 4500
001			vtls000003890
003			VRT
005			20250102223208.0
008			090107s2007 maua |b 001 0 eng
020			_a0071254080 (IE)
039		9	_a201402040120 _bVLOAD _c201007211211 _dmalmash _c200901201333 _dvenkatrajand _c200901070913 _dvenkatrajand _y200901070913 _zvenkatrajand
050		4	_aTL570 _b.A677 2007
100	1		_aAnderson, John David. _918625
245	1	0	_aFundamentals of Aerodynamics / _cJohn D. Anderson, Jr.
250			_a4th ed.
260			_aBoston, Mass. ; _aLondon : _bMcGraw-Hill, _cc2007.
300			_axxiv, 1008 p. : _bill. ; _c24 cm.
440		0	_aMcGraw-Hill series in aeronautical and aerospace engineering _918626
504			_aIncludes bibliographical references (p. 877-881) and index.
505			_aPart 1 Fundamental Principles1 Aerodynamics: Some Introductory Thoughts2 Aerodynamics: Some Fundamental Principles and EquationsPart 2 Inviscid, Incompressible Flow3 Fundamentals of Inviscid, Incompressible Flow4 Incompressible Flow over Airfoils5 Incompressible Flow over Finite Wings6 Three-Dimensional Incompressible FlowPart 3 Inviscid, Compressible Flow7 Compressible Flow: Some Preliminary Aspects8 Normal Shock Waves and Related Topics9 Oblique Shock and Expansion Waves10 Compressible Flow Through Nozzles, Diffusers, and Wind Tunnels11 Subsonic Compressible Flow over Airfoils: Linear Theory12 Linearized Supersonic Flow13 Introduction to Numerical Techniques for Nonlinear Supersonic Flow14 Elements of Hypersonic FlowPart 4 Viscous Flow15 Introduction to the Fundamental Principles and Equations of Viscous Flow16 Some Special Cases; Couette and Poiseuille Flows17 Introduction to Boundary Layers18 Laminar Boundary Layers19 Turbulent Boundary Layers20 Navier-Stokes Solutions: Some ExamplesAppendix A Isentropic Flow PropertiesAppendix B Normal Shock PropertiesAppendix C Prandtl-Meyer Function and Mach AngleAppendix D Standard Atmosphere, SI UnitsAppendix E Standard Atmosphere, English Engineering Units
520			_aIn keeping with its bestselling previous editions, Fundamentals of Aerodynamics, fourth edition, offers the most readable, interesting, and up-to-date overview of aerodynamics to be found in any text. The classic organization of the text has been preserved, with new stand-alone viscous flow sections at the end of various chapters to conceptualize the coverage of this topic in part 4, and complement discussion of fundamental principles in part 1, inviscid incompressible flow in part 2, and inviscid compressible flow in part 3. Historical topics, carefully developed examples, numerous illustrations, and a wide selection of chapter problems are found throughout the text to motivate and challenge students of aerodynamics.
650		0	_aAerodynamics. _912193
942			_2lcc _n0 _cBK
999			_c7243 _d7243