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FLUGTURBINE
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Air force facility for large turbine engine compressor testing
Airline economic benefit through engine development
Current and future use of an AIDS integrated EMS
Low emission, water-tolerant combustor for a small, all-weat er turboshaft gas turbine engine
Application of the Semi-Loof thin shell element to the analysis of aircraft engine structures
Trends in high temperature materials technology for advanced aircraft turbine engines
Effect of broadened-specification fuels on aircraft engines and fuel systems
Powder metallurgical innovations for improved hot section alloys in aero-engine applications
Regression techniques applied to parametric turbine engine simulations
Reliability prediction techniques for second generation marine and industrial gas turbines
State of the art in aircraft gas turbine technology
Fiber-reinforced composites: the future for aeropropulsion
Aircraft gasturbine cycle programs - requirements for compressor and turbine performance prediction
First refraction enhanced 3D computed tomography. Application to metal matrix composites
Inlet-engine compatibility testing techniques in ground test facilities
Applied reliability/maintainability methodology as a function within life cycle cost
A study on the mechanism of compressor surge due to inlet pressure disturbances
Aerostructural considerations for the power plant of overlapping wing configuration
Zerspantechnik in zukunftsfähigen Industrien
Calculated rotordynamik behaviour of a twin spool engine and the comparison with the results
WHIPOX: ein Leichtbauwerkstoff für Hochtemperaturanwendungen
Dispersion strengthened aluminium: potential for service at and above 400 Cel
The application of modal analysis to the fault diagnosis of aeroengines
Jet engine fan blade containment using two alternate geometries
Service experience and materials evolution in air force jet engines
Some unconventional aero gas turbines using hydrogen fuel
Development of gas turbine performance seeking logic
Full-scale aircraft turbine engine controlled environment corrosion testing
Konstruktive Gestaltung von CMC-Brennkammerschindeln
Design concepts for low cost composite engine frames
Condition monitoring experience on CF6 engines
A novel concept for suppressing internally generated aircraft engine noise
Recent advancements in turbomachinery forced response analyses
NASA broad-specification fuels combustion technology programstatus and description