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Turboluftstrahltriebwerk
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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
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
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
A neural network model for UAV propulsion system
Practical near hover flight control of a ducted fan (SLADe)
Aerodynamic performance of a bypass engine with fan nozzle exit area change by warped chevrons
Fundamentals of jet propulsion with power generation applications
Vibration fault identification of a turbojet engine based on cepstrum analysis
Fuel effects on operability of aircraft gas turbine combustors
Simulation-based dynamic model and speed controller design of a small-scale turbojet engine
Engine and multitask airplane integration: criteria of engine parameters selection
Analysis of low-thrust liquid rocket engines with a methane air pump unit
Fatigue Damage Modeling Approach Based on Evolutionary Power Spectrum Density
FENSAP-ICE Modeling of the Ice Particle Threat to Engines in Flight
Diode-laser sensor for air-mass flux 2: Nonuniform flow modeling and aeroengine tests
Untersuchungen zur Leistungsverschlechterung von Turboluftstrahltriebwerken
Design optimization of a mixed-flow compressor impeller for a small turbojet engine
Electromagnetic Interference on Aircraft from Jet Engine Charging
Noise analysis of the turbojet and turbofan engine tests
Schubumkehrer System Integration SuSI bei einem Turboflugtriebwerk : Anschlußbericht Projekt SuSI
Schubumkehrer System Integration SuSI bei einem Turboflugtriebwerk : Anschlußbericht Projekt SuSI
Turbojet and turbofan engines for a mach 3 supersonic transport
Applying Protective Coating on the Turbine Engine Turbine Blades by Means of Plasma Spraying
Determination of the flight trajectory in terms of emission and fuel consumption minimization
The laboratory test rig with miniature jet engine to research aviation fuels combustion process
Numerical Investigation of Ice Shedding Associated with Engine Fan Icing
Turbofan aft noise predictions based on Lilley's wave model
Turbojet Engine Parameters Calculation Based on Fuel Flow and Exhaust Gas Temperature