Abschlussbericht LuFo 3 : VIT (virtuelles Triebwerk) ; Berichtszeitraum: Oktober 2003 - Februar 2007
Advanced airbreathing propulsion cycles for high speed flight
Aerodynamic assessment of methods to simulate flight inflow characteristics during static testing
Aerodynamic design and performance of an over-wing low pressure ratio fan stage
Aerodynamic design and performance of an over-wing low pressure ratio fan stage
Aeroegine [i.e. aeroengine] noise : December 2 - 4, 2014
Aeroengines for regional airline aircraft : abstract of lectures
Aircraft drag reduction, the application of natural laminar flow to aero-engine nacelles
Aircraft engines join thrust for lower emission levels
Airframe and powerplant mechanics powerplant written test guide
Aktive Beeinflussung von Sekundärströmungen an einer Verdichterkaskade mit Synthetik-Jet-Aktuatoren
Analyse und Vergleich fertigungstechnischer Prozessketten für Flugzeugtriebwerks-Rotoren
Analyse und Vergleich fertigungstechnischer Prozessketten für Flugzeugtriebwerks-Rotoren
ANALYSIS OF A COMPACT COMBUSTOR FOR USE IN A JETCAT P90 RXI
ANALYSIS OF DISTORTION PHASE SHIFT IN A HIGHLY LOADED FAN STAGE
ANALYSIS OF GAS TURBINE COOLING TECHNOLOGIES FOR HIGHER NATURAL GAS COMBINED CYCLE EFFICIENCY
ANALYSIS OF THE IMPACT OF CONTROL METHODS ON TURBOFAN PERFORMANCE IN ICE CRYSTAL CONDITIONS
ANALYSIS OF TURBINE VISCOUS FLOW USING A NOVEL PROPER ORTHOGONAL DECOMPOSITION METHOD
An analysis of opportunistic maintenance policy for the F100PW100 aircraft engine
AN ASSESSMENT OF EQUATION-OF-STATE FOR SUPERCRITICAL COMBUSTION SYSTEMS
AN AUTOMATED ANALYTICAL DIFFERENTIA TION FRAMEWORK FOR REACTING FLOW SIMULATION
An integrated economic evaluation of preliminary aero-engine design concepts
AN INVESTIGATION INTO THE FEASIBILITY OF ALTERNATIVE AVIATION FUELS
AN INVESTIGATION OF COOLED COOLING AIR FOR A MACH 2.2 COMMERCIAL SUPERSONIC TRANSPORT
APPLICATION OF A COMPACT COMBUSTOR IN SMALL-SCALE JETCAT ENGINES
Application of Navier-Stokes methods for engine/airframe integration
A ROBUST INITIALIZATION APPROACH OF MULTI-POINT SYNTHESIS SCHEMES FOR AERO-ENGINE CONCEPTUAL DESIGN