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FLUGTURBINE
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Abrasive-waterjet machining of ceramic-coated materials
Active control of noise from turbomachines - control algorithms and experimental results
Advanced airbreathing propulsion cycles for high speed flight
Aerodynamic and thermodynamic characteristics of flow fields below VTOL vehicles in ground proximity
Aerodynamic components for small turboshaft engines
Aerodynamic performance of acoustically suppressed exhaust nozzles
Aerostructural considerations for the power plant of overlapping wing configuration
A family of small, low cost turbojet eingines for short life applications
AFWAL turbine engine controls research and development - Present and future
Aircraft gasturbine cycle programs - requirements for compressor and turbine performance prediction
Aircraft turbine engine combustors - development status/challenges
Air cycle air conditioning of turbine powered helicopters
Air force facility for large turbine engine compressor testing
Airline economic benefit through engine development
A model-based monitoring system for turbine engines
A multi-purpose airborne integration display and data collection system for monitoring jet engines
Analysis of weak glancing shock/boundary layer interactions
Analytical algorithm for the design of valve contours
Analytic model of MPM 20 engine depicted within characteristics of its compressor
An early glimpse at long term subsonic commercial turbofan technology requirements
An empirical model for the mixing of a row of dilution jets with confined crossflow
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 considerations for integral gas turbine electric starter/generator revisited
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
Approaches to improving aircraft efficiency
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
Assessment of the structural-mechanical design of commercial aircraft gas turbine engines
A study on the mechanism of compressor surge due to inlet pressure disturbances
Automated repair and overhaul of aero-engine and industrial gas turbine components
Basic ignition research related to altitude relight problems
Beamforming on a turbofan engine in an indoor test-facility
Biologically inspired motors for micro-air-vehicles
Calculated rotordynamik behaviour of a twin spool engine and the comparison with the results
Calculations of hot gas ingestion for a STOVL aircraft model
Characteristics of aeroelastic instabilities in turbomachinery - NASA full scale engine test results
Combustor concepts for aircraft gas turbine low-power emissions reduction