The energy-autonomous cabin - the end of classical on-board power supply?
"Buzz-saw" noise: Prediction of the rotor-alone pressure field
Wenn die Asche schmilzt. Die Chemie zwischen Vulkan und Triebwerk
Dehn-Schrumpf-Verband an einem hochtourig drehenden skalierten Flugtriebwerks-Rotor
Experimental study of flow behaviour and thermal loads in dual bell nozzles
Experimental investigation of engine jet-vortex interaction
Experimentelle Untersuchungen zur Grenzschichtbeeinflussung hochbelasteter Niederdruckturbinen
Torsional vibration of crankshaft in an engine-propeller nonlinear dynamical system
Luftfahrtforschungsprogramm 'Unterflügelantriebsinstallation'. Abschlußbericht
Associations between factors influencing engineering design communication
On the drag of isolated axisymmetric carbon fibre composite engine nacelles at zero incidence
Active trim panel attachments for control of sound transmission through aircraft structures
Vibration damping of aero engine rotors by elastomer ring bearings
Factory and process simulation in aero-engine component manufacturing
Post-combustion evolution of soot properties in an aircraft engine
Herstellung und Eigenschaften von Superlegierungen mit zellularem Gefügeaufbau
Engine design and operational impacts on particulate matter precursor emissions
Untersuchung des Entzündungsbereiches des Kraftstoffes in der Brennkammer
Performance analysis of helicopter development engine using a synthesis model and soft computing
On the prediction of 'buzz-saw' noise in aero-engine inlet ducts
Time-domain simulation of acoustic propagation in a lined duct
Metal injection moulding for manufacturing aeroengine components
Ein Name bürgt weltweit für Erfolg. IAE International Aero Engines AG
Interdisciplinary design for aero-mechanical interaction in modern turbomachinery
Interference phenomena of upper-wing-mounted engines
Development of the S-76B/PT6B-36B engine acceleration schedule
Application of Navier-Stokes methods for engine/airframe integration
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