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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
Airline economic benefit through engine development
Aerodynamic performance of a bypass engine with fan nozzle exit area change by warped chevrons
Simulated mission endurance test (SMET) for an aircraft engine to be used in a fighter/attack role
Low emission, water-tolerant combustor for a small, all-weat er turboshaft gas turbine engine
Trends in high temperature materials technology for advanced aircraft turbine engines
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
Reliability prediction techniques for second generation marine and industrial gas turbines
The economic efficiency of raising the flying life and reliability of gas-turbine engines
Small turbine engine performance evaluation of high density fuels. Part I. Blends of RJ-5 fuel
State of the art in aircraft gas turbine technology
Fiber-reinforced composites: the future for aeropropulsion
NASA-Programm zur Senkung des Bedarfs an Kobalt, Niob, Chrom und Tantal
AGARD-LS-83 Series 83. Modern prediction methods for turbomachine performance
Small turbine engine noise reduction. Volume 1: Executive summary
First refraction enhanced 3D computed tomography. Application to metal matrix composites
Perspektiven der Verwendung von Wasserstoff in Gasturbinentriebwerken
Aircraft gasturbine cycle programs - requirements for compressor and turbine performance prediction
Inlet-engine compatibility testing techniques in ground test facilities
Calculated rotordynamik behaviour of a twin spool engine and the comparison with the results
Advanced technology components for model GTP 305-2 aircraft auxiliary power system