000 01448mm a2200409a 44500
001 NM003185
003 AR-HaUTN
007 ta
008 43020sc. 1 ||||||||||||||000 | spa||
005 20240912185434.0
040 _aarhautn
100 _aVavra, M. H.
_97929
245 _aAero-thermodynamics and flow in turbomachines
_cM. H. Vavra
250 _a[1st?] ed.
260 _aNew York
_bJohn Wiley
300 _a609 p.
_bgráficos
505 _tKinematics of fluid particles
505 _tGeneral stress conditions of fluid particle
505 _tEquation of motion
505 _tEnergy equation
505 _tMomentum theorem
505 _tLow of moment of momentum
505 _tRelative motions
505 _tRotational motion
505 _tIsentropic flow of perfect gases
505 _tPotential flows
505 _tAxisymmetric flows in rotating and stationary passages
505 _tQuasi two-dimensional flows in turbomachines
505 _tAxial flow compressor stages
505 _tTwo-dimensional potential flow through arbitrary cascades
505 _tOne-dimensional flow through turbine stages
505 _tSimplified three-dimensional analysis of axial turbomachines
505 _tReview of vector analysis [Appendix A]
505 _tIntroduction to operations involving dyadics [Appendix B]
505 _tTables of optimun operating conditions of axial turbine stages [Appendix C]
942 _cBK
999 _c3185
_d3185