000			02337mm a2200541a 44500
001			NM002600
003			AR-HaUTN
007			ta
008			11120s2010 ||||||||||||||000 | spa||
005			20240917164213.0
020			_a9781848211414
040			_aAR-HaUTN
100			_aDélery, Jean _97406
245			_aHandbook of compressible aerodynamics _cJean Délery
250			_a1st ed.
260			_aHoboken _bJohn Wiley
300			_axxiii, 744 p.
500			_aApéndices e índice alfabético, al final del libro
504			_aReferencias bibliográficas p. 733738
505			_tAerodynamics : aims, areas of application and current issues
505			_tAerodynamic forces : basic definitions
505			_tReview of thermodynamics
505			_tFundamental equations of fluid mechanics
505			_tFirst applications of the conservation equations
505			_tDimensionless equations : similarity parameters
505			_tClassification of flows
505			_tFundamental concepts of fluid mechanics
505			_tOnedimensional, nonviscous and adiabatic steady flows
505			_tApplication of the onedimensional theory to the calculation of supersonic nozzles
505			_tOnedimensional flows with friction and heat transfer
505			_tApplications of the onedimensional theory to the calculation of supersonic ejectors
505			_tDiscontinuity surfaces : shock wave and slip line
505			_tOblique Shock wave and shock polar
505			_tShock intersections or shockshock interferences
505			_tApplication of the shock wave theory to supersonic air intakes
505			_tSupersonic, steady, twodimensional flows and the theory of characteristics
505			_tThe numerical method of characteristics
505			_tApplication of the method of characteristics to the calculation of supersonic nozzles
505			_tFlows with stock waves : rotational method of characteristics
505			_tOnedimensional, non viscous and adiabatic unstedy flows
505			_tUnsteady shock wave, contact surface, and wave reflections
505			_tShock tube
505			_tNumerical methods for calculating unsteady flows
505			_tSome properties of transonic flows
653			_aINGENIERIA AERONAUTICA
653			_aPROYECTO Y DISENO AERODINAMICO
942			_cBK
999			_c2600 _d2600