000			01977nam a22003978i 4500
001			CR9781316389331
003			UkCbUP
005			20200124160157.0
006			m|||||o||d||||||||
007			cr||||||||||||
008			150219s2019||||enk o ||1 0|eng|d
020			_a9781316389331 (ebook)
020			_z9781107123052 (hardback)
040			_aUkCbUP _beng _erda _cUkCbUP
050	0	0	_aQA930 _b.K5875 2019
082	0	0	_a533/.62 _223
100	1		_aKnight, Doyle, _eauthor.
245	1	0	_aEnergy deposition for high-speed flow control / _cDoyle D. Knight.
264		1	_aCambridge : _bCambridge University Press, _c2019.
300			_a1 online resource (x, 450 pages) : _bdigital, PDF file(s).
336			_atext _btxt _2rdacontent
337			_acomputer _bc _2rdamedia
338			_aonline resource _bcr _2rdacarrier
490	1		_aCambridge aerospace series ; _v47
500			_aTitle from publisher's bibliographic system (viewed on 12 Feb 2019).
520			_aWritten by a leading expert in the field, this book presents a novel method for controlling high-speed flows past aerodynamic shapes using energy deposition via direct current (DC), laser or microwave discharge, and describes selected applications in supersonic and hypersonic flows. Emphasizing a deductive approach, the fundamental physical principles provided give an understanding of the simplified mathematical models derived therefrom. These features, along with an extensive set of 55 simulations, make the book an invaluable reference that will be of interest to researchers and graduate students working in aerospace engineering and in plasma physics.
650		0	_aAerodynamics.
650		0	_aGas dynamics.
650		0	_aAir flow.
650		0	_aFluid dynamics.
650		0	_aElectric discharges.
650		0	_aSurface discharges (Electricity)
776	0	8	_iPrint version: _z9781107123052
830		0	_aCambridge aerospace series ; _v47.
856	4	0	_uhttps://doi.org/10.1017/9781316389331
999			_c514511 _d514509