Research trends and opportunities in air breathing propulsion
Aerodynamic assessment of methods to simulate flight inflow characteristics during static testing
Discrete vortex modelling of an axisymmetric jet flowfield
A unique coannular plug nozzle jet noise prediction procedure
Propeller light aircraft noise at discrete frequencies
Prediction of the interior noise levels of high-speed propeller-driven aircraft
Engine aerodynamic installation by numerical simulation
The oil/air system of a modern fighter aircraft engine
Rechnerische Untersuchung des Schwingungsverhaltens eines hochtourigen Rotors
Ceramic applications in turbine engines (CATE) program summary
Large-scale advanced propfan (LAP) program progress report
Benefits of blade sweep for advanced turboprops
Design and life assessment of aeroengine components
Aircraft drag reduction, the application of natural laminar flow to aero-engine nacelles
Hybrid laminar flow technology for aero-engine nacelles
Implications of low emissions requirements on aircraft engine design and flight operations
Synergism between corrosion and fatigue of Al 2024-T3 alloy
Interference phenomena of upper-wing-mounted engines
Application of Navier-Stokes methods for engine/airframe integration
Interdisciplinary design for aero-mechanical interaction in modern turbomachinery
Metal injection moulding for manufacturing aeroengine components
Factory and process simulation in aero-engine component manufacturing
Post-combustion evolution of soot properties in an aircraft engine
Engine design and operational impacts on particulate matter precursor emissions
Vibration damping of aero engine rotors by elastomer ring bearings
Shunt loudspeaker technique for use as acoustic liner
DETERMINATION OF NITRIC OXIDE CONCENTRATIONS IN MIXTURES WITH NITROGEN TETROXIDE VIA IR SPECTROMETRY
INVESTIGATION OF COMBUSTION INSTABILITIES IN A FULL FLOW STAGED COMBUSTION MODEL ROCKET COMBUSTOR
STUDIES ON FLAME SPREAD ACCELERATION, DETONATION KERNEL IN A DUAL-THRUST ROCKET
PILOT INJECTOR REDESIGN TO REDUCE N+3 CYCLE EMISSIONS FOR A GAS-TURBINE COMBUSTOR
COMBUSTION BEHAVIOR OF AMMONIUM PERCHLORATE AT HIGH PRESSURES