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FLUGTURBINE
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Foaming characteristics of MIL-L-7808 turbine lubricants
Air force facility for large turbine engine compressor testing
High temperature attack of Nimonic 80 A by vanadium
Factors controlling pollutant emissions from gas turbine engines
A new approach in turbomachinery flow analysis using the finite element method
Aerodynamic performance of a bypass engine with fan nozzle exit area change by warped chevrons
Low emission, water-tolerant combustor for a small, all-weat er turboshaft gas turbine engine
Powder metallurgical innovations for improved hot section alloys in aero-engine applications
Jet engine coatings for resisting volcanic ash damage
Goodman diagram via vibration-based fatigue testing
Modeling of subsonic flow through a compact offset inlet diffuser
Effect of broadened-specification fuels on aircraft engines and fuel systems
Application of the Semi-Loof thin shell element to the analysis of aircraft engine structures
Fiber-reinforced composites: the future for aeropropulsion
State of the art in aircraft gas turbine technology
Small turbine engine performance evaluation of high density fuels. Part I. Blends of RJ-5 fuel
NASA-Programm zur Senkung des Bedarfs an Kobalt, Niob, Chrom und Tantal
AGARD-LS-83 Series 83. Modern prediction methods for turbomachine performance
First refraction enhanced 3D computed tomography. Application to metal matrix composites
Small turbine engine noise reduction. Volume 1: Executive summary
Perspektiven der Verwendung von Wasserstoff in Gasturbinentriebwerken
Inlet-engine compatibility testing techniques in ground test facilities
Aircraft turbine engine fuel corrosion inhibitors and their effects on fuel properties
Calculated rotordynamik behaviour of a twin spool engine and the comparison with the results
Zerspantechnik in zukunftsfähigen Industrien
Ruß ist nicht gleich Ruß. Partikelmessungen an Flugzeugantrieben
Innovative approach to air management strategy for turbocharged diesel aircraft engines
A study on the mechanism of compressor surge due to inlet pressure disturbances
Aerostructural considerations for the power plant of overlapping wing configuration
Dispersion strengthened aluminium: potential for service at and above 400 Cel
WHIPOX: ein Leichtbauwerkstoff für Hochtemperaturanwendungen
Small turbine engine noise reduction. Volume 2: Noise prediction methods
The application of modal analysis to the fault diagnosis of aeroengines