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Flugtriebwerk
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Some Design Considerations for Two-Dimensional, Mixed-Compression Inlets for Mach 2.5 to 3.5
Assessment of Engine Modelling on the Installed Aerodynamics of an Ultra-High Bypass Turbofan
Robust Design Under Uncertainty of Hypersonic Inlets
CFD Simulation of Ground Vortex Intake Test Case Using ANSYS FLUENT
Adjoint Based Shape Optimization of an S-Shaped Duct with SU2
Comparison of Nacelle Models for the Evaluation of an Ultra-High Bypass Engine Aerodynamics
Propellants and combustion / American Institute of Aeronautics and Astronautics ; Volume 1 of 2
Computational Analysis of an Inlet Ground Vortex Test Case Using CFD++
Effect of Farfield Boundary on Simulations of the Inlet in Crossflow
Comparison of CFD Ground Vortex Results with the 5th PAW Intake Near the Ground Experiment
Entwurfsmethode für elektrische und hybride Kleinflugzeugantriebe