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FLUGTURBINE
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Abrasive-waterjet machining of ceramic-coated materials
Active control of fan noise from a turbofan engine
Advanced technology components for model GTP 305-2 aircraft auxiliary power system
Aerodynamic and thermodynamic characteristics of flow fields below VTOL vehicles in ground proximity
Aerodynamic performance of a bypass engine with fan nozzle exit area change by warped chevrons
Aerostructural considerations for the power plant of overlapping wing configuration
AGARD-LS-83 Series 83. Modern prediction methods for turbomachine performance
Aircraft gasturbine cycle programs - requirements for compressor and turbine performance prediction
Aircraft turbine engine combustors - development status/challenges
Aircraft turbine engine fuel corrosion inhibitors and their effects on fuel properties
Air force facility for large turbine engine compressor testing
Airline economic benefit through engine development
Airplane responsive engine selection (ARES). Volume I. ARES user guide
Aluminium-Hochleistungswerkstoffe durch mechanisches Legieren und Reaktionsmahlen. T. 2
Analysis of weak glancing shock/boundary layer interactions
Analytical algorithm for the design of valve contours
A new approach in turbomachinery flow analysis using the finite element method
An investigation of the induced aerodynamic effects of a vectored non-axisymmetric exhaust nozzle
A novel concept for suppressing internally generated aircraft engine noise
Application of the Semi-Loof thin shell element to the analysis of aircraft engine structures
Application of unsteady aerodynamics and aeroelasticity in heavy-duty gas turbines
Applied reliability/maintainability methodology as a function within life cycle cost
A review of NASA's propulsion programs for civil aviation
A rotating stall control system for turbojet engines
A small perturbation theory for supersonic jets
A study on the mechanism of compressor surge due to inlet pressure disturbances
Auf dem Weg zu einem probabilistischen Lebensdauermodell für Flugturbinenscheiben
Besonderheiten der experimentellen Absicherung bei der Entwicklung moderner Flugzeugtriebwerke
Blade loss transient dynamic analysis of turbomachinery
Blade tip timing and strain gauge correlation on compressor blades
Calculated rotordynamik behaviour of a twin spool engine and the comparison with the results
Ceramic bearings for use in gas turbine engines
Chaotic response of panel vibrations forced by turbulent boundary layer and sound
Chinese technology. Overview: Investment casting alloys for aircraft parts
Collocates structural control for reduction of aircraft cabin noise
Combustor concepts for aircraft gas turbine low-power emissions reduction