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Turboluftstrahltriebwerk
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Study of performance of the aircraft gas turbine engine integrated with a gas dynamic laser
Study of performance of the aircraft gas turbine engine integrated with a gas dynamic laser
Integration of a High-Pressure Gas Turbine of the Gas Turbine Engine with a Gas-Dynamic Laser
Integration of a High-Pressure Gas Turbine of the Gas Turbine Engine with a Gas-Dynamic Laser
Separating turbofan engine noise sources using auto- and cross spectra from four microphones
Multi-objective optimization for centrifugal compressor of mini turbojet engine
Parametric and nonparametric system identification of an experimental turbojet engine
Practical near hover flight control of a ducted fan (SLADe)
A neural network model for UAV propulsion system
Aerodynamic performance of a bypass engine with fan nozzle exit area change by warped chevrons
Vibration fault identification of a turbojet engine based on cepstrum analysis
Fundamentals of jet propulsion with power generation applications
Engine and multitask airplane integration: criteria of engine parameters selection
Simulation-based dynamic model and speed controller design of a small-scale turbojet engine
Untersuchungen zur Leistungsverschlechterung von Turboluftstrahltriebwerken
Diode-laser sensor for air-mass flux 2: Nonuniform flow modeling and aeroengine tests
Analysis of low-thrust liquid rocket engines with a methane air pump unit
Fatigue Damage Modeling Approach Based on Evolutionary Power Spectrum Density
Turbofan aft noise predictions based on Lilley's wave model
Schubumkehrer System Integration SuSI bei einem Turboflugtriebwerk : Anschlußbericht Projekt SuSI
Schubumkehrer System Integration SuSI bei einem Turboflugtriebwerk : Anschlußbericht Projekt SuSI
FENSAP-ICE Modeling of the Ice Particle Threat to Engines in Flight
Design optimization of a mixed-flow compressor impeller for a small turbojet engine
Noise analysis of the turbojet and turbofan engine tests
Turbojet and turbofan engines for a mach 3 supersonic transport
Electromagnetic Interference on Aircraft from Jet Engine Charging
Applying Protective Coating on the Turbine Engine Turbine Blades by Means of Plasma Spraying
The laboratory test rig with miniature jet engine to research aviation fuels combustion process
Numerical Investigation of Ice Shedding Associated with Engine Fan Icing
Ice-Crystal Icing Accretion Studies at the NASA Propulsion Systems Laboratory