Particle Dynamics Simulation for Aeroengine Intake Design

The design of an engine intake comprising an inertial inlet particle separator is accomplished under this work. With that purpose a Navier Stokes solver is used for aerodynamics performance investigation for design and off design conditions and the particle trajectories are obtained using a post pro...

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Bibliographische Detailangaben

Hauptverfasser:	DE LA Calzada, P, Vazquez, R, Fernandez, F, San Segundo, M P
Format:	Report
Sprache:	eng
Schlagworte:	AERODYNAMICS AIRCRAFT ENGINES COMPUTATIONAL FLUID DYNAMICS Fluid Mechanics FOREIGN REPORTS IPS(INLET PARTICLE SEPARATORS) Jet and Gas Turbine Engines NAVIER STOKES EQUATIONS PARTICLE DYNAMICS PARTICLE SIZE PARTICLE TRAJECTORIES REYNOLDS NUMBER SPAIN TURBOPROP ENGINES
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