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Flugtriebwerk
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2D SCALING EFFECTS ON INERTIAL PARTICLE SEPARATOR PERFORMANCE
9th CEAS European Propulsion Forum : Roma, Italy, October 15 - 17, 2003
A CFD INVESTIGATION OF A DIVERTERLESS SUPERSONIC INLET OF ELLIPSOIDAL ENTRANCE SHAPE
Adjoint Based Shape Optimization of an S-Shaped Duct with SU2
Advanced Parametric Lobe Mixer Concepts for Internally Mixed Nozzles
Advanced propulsion systems and technologies, today to 2020
AERODYNAMIC BEHAVIOR OF A COUPLED BOUNDARY LAYER INGESTING INLET — DISTORTION TOLERANT FAN
Aerodynamic design and performance of an over-wing low pressure ratio fan stage
AERODYNAMIC SHAPE OPTIMIZATION OF AIRCRAFT ENGINE NOZZLES BASED ON COMPUTER-AIDED DESIGN
Aerodynamics of a Compact Nacelle at Take-Off Conditions