000			02091nam a22003258i 4500
001			CR9781316014288
003			UkCbUP
005			20200124160210.0
006			m|||||o||d||||||||
007			cr||||||||||||
008			140325s2017||||nyu o ||1 0|eng|d
020			_a9781316014288 (ebook)
020			_z9781107082700 (hardback)
040			_aUkCbUP _beng _erda _cUkCbUP
050	0	0	_aQC168 _b.C487 2017
082	0	0	_a533/.2 _223
100	1		_aChen, Ruey-Hung, _eauthor.
245	1	0	_aFoundations of gas dynamics / _cRuey-Hung Chen.
264		1	_aNew York : _bCambridge University Press, _c2017.
300			_a1 online resource (x, 418 pages) : _bdigital, PDF file(s).
336			_atext _btxt _2rdacontent
337			_acomputer _bc _2rdamedia
338			_aonline resource _bcr _2rdacarrier
500			_aTitle from publisher's bibliographic system (viewed on 14 Apr 2017).
520			_aFoundations of Gas Dynamics covers supersonic and subsonic flow phenomena where compressibility of the fluid cannot be ignored. It finds application in jet and rocket propulsion systems as well as handling industrial gas flow at high speeds. Students and engineers in the mechanical, aerospace, and chemical disciplines will find it useful. It begins with basic concepts such as isentropic flows, shock, and supersonic expansion waves in one dimension. These are followed by one-dimensional flows with friction and heat exchange. Two-dimensional theory with small perturbations is presented, with its applications illustrated by supersonic airfoils. Method of characteristics is used for flows with two independent variables, either with two spatial coordinates or with time variations in one dimension. In later chapters, acoustic wave propagation, supersonic flow combustion, and unsteady shock formation are treated thoroughly. The book ends with a chapter on basic hypersonic flow, with a discussion of similarity rules.
650		0	_aGas dynamics.
650		0	_aGases _xThermal properties.
776	0	8	_iPrint version: _z9781107082700
856	4	0	_uhttps://doi.org/10.1017/9781316014288
999			_c515671 _d515669