Synonyme wurden verwendet für:
Flugzeuggasturbine
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keywords:(Flugzeuggasturbine)
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
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
Vibration fault identification of a turbojet engine based on cepstrum analysis
Engine and multitask airplane integration: criteria of engine parameters selection
Simulation-based dynamic model and speed controller design of a small-scale turbojet engine
Analysis of low-thrust liquid rocket engines with a methane air pump unit
Untersuchungen zur Leistungsverschlechterung von Turboluftstrahltriebwerken
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
Applying Protective Coating on the Turbine Engine Turbine Blades by Means of Plasma Spraying
Turbojet and turbofan engines for a mach 3 supersonic transport
The laboratory test rig with miniature jet engine to research aviation fuels combustion process
EXPERIMENTAL SEA-LEVEL STATIC INVESTIGATION OF A SHORT AFTERBURNER
An acceleration schedule control for accelerating a turbojet engine and its use with a speed control
Considerations of hot-gas ingestion for jet V/STOL aircraft
Altitude Performance of a Turbojet Engine Using Pentaborane Fuel
Influence of boric oxide deposition on turbojet-engine operation
A low-pressure-loss short afterburner for sea-level thrust augmentation
Conceptual approach to design of materials for GTE turbine blades
Conceptual approach to design of materials for GTE turbine blades
Erkennung und Vermeidung von Verdichterinstabilitäten am Turbostrahltriebwerk Larzac 04
Analysis of domestic aircraft gas turbine engine development dynamics
Analysis of domestic aircraft gas turbine engine development dynamics