000			01581cam a22002298i 4500
001			10876
003			IN-BhIIT
005			20240702152415.0
008			190124s2019 nju b 001 0 eng
020			_a9781119580560
040			_aIN-BhIIT
041			_aeng
082	0	0	_a629.1323 _bCHI/M
100	1		_aChin, Wilson C., _eAuthor. _923691
245	1	0	_aModern aerodynamic methods for direct and inverse applications / _cby Wilson C. Chin.
260			_aBeverly, M.A : _bScrivener Publishing, _c2019.
300			_axiv, 426 p. : _bill. ; _c24 cm.
504			_aIncludes bibliographical references and index.
520			_aThis book helps readers approach the literature more critically. Rather than simply understanding an approach, for instance, the powerful "type differencing" behind transonic analysis, or the rationale behind "conservative" formulations, or the use of Euler equation methods for shear flow analysis when they are unnecessary, the author guides and motivates the user to ask why and why not and what if. And often, more powerful methods can be developed using no more than simple mathematical manipulations. For example, Cauchy-Riemann conditions, which are powerful tools in subsonic airfoil theory, can be readily extended to handle compressible flows with shocks, rotational flows, and even three-dimensional wing flowfields, in a variety of applications, to produce powerful formulations that address very difficult problems. This breakthrough volume is certainly a "must have" on every engineer's bookshelf.
650		0	_aAerodynamics.
942			_cTRB
999			_c13842 _d13842