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001			NM000421
003			AR-HaUTN
007			ta
008			78020sc. 1 ||||||||||||||000 | spa||
005			20240917164003.0
020			_a1563472414
040			_aAR-HaUTN
100			_aOates, Gordon C. _93986
245			_aAerothermodynamics of gas turbine and rocket propulsion _cGordon C. Oates
250			_a3rd. ed.
260			_aReston _bAmerican Institute of Aeronautics and Astronautics
300			_axii, 456 p. _bgráficos _e1 disco compacto
490			_aAIAA Education Series
500			_aApéndices e índice alfabético, al final del libro
500			_aEl material complementario contiene un software con los problemas y diseños estudiados en el libro
505			_tIntroduction
505			_tThermodynamics and quasione dimensional fluid flows
505			_tChemical rockets
505			_tNonchemical rockets
505			_tIdeal cycle analysis
505			_tComponente performance
505			_tNonideal cycle analysis
505			_tEngine offdesign performance
505			_tElementary theory of blade aerodynamics
505			_tTroughflow theory
505			_tCascade flows
800			_aPrzemieniecki, J. S. _93987
942			_cBK
999			_c421 _d421