Ölfeuer in Flugtriebwerken : Selbstentzündung und Flammenausbreitung
On the drag of isolated axisymmetric carbon fibre composite engine nacelles at zero incidence
On the mechanisms of combustion driven low-frequency oscillations in aero-engines
On the prediction of 'buzz-saw' noise in aero-engine inlet ducts
Optical diagnostics for reacting and non-reacting flows : theory and practice
OPTIMAL SENSOR PLACEMENT FOR AZIMUTHAL ACOUSTIC MODE IN CYLINDRICAL DUCTS
Optimierung der Architektur moderner ziviler Flugtriebwerke zur Verbesserung der Lebenswegkosten
Optimierung der Spiele und Spalte im Konstruktionsprozess von Flugtriebwerken
OPTIMIZATION ALGORITHM FOR AXIAL MULTISTAGE COMPRESSOR WORKFLOYW
OPTIMIZATION OF AN AIR TURBOSTARTER OF A LAUNCH SYSTEM FOR GAS TURBINE ENGINE
PARAMETRIC DESIGN OPTIMIZATION IN COMPUTATIONAL AERODYNAMICS USING ARTIFICIAL DEEP NEURAL NETWORKS
PARAMETRIC STUDIES OF SWIRL COMBUSTOR USING LES: THE EFFECT OF INJECTORS' ANGLE
PARAMETRIC STUDY OF A TURBOJET ENGINE WITH AUXILIARY BYPASS COMBUSTION - THE TURBOAUX ENGINE
Performance analysis of helicopter development engine using a synthesis model and soft computing
POSSIBLE EFFECTS OF TURBINE/FUEL CELL INTEGRATION ON COMBUSTOR OPERATION
Post-combustion evolution of soot properties in an aircraft engine
PRELIMINARY EXPERIMENTATION ON WALL BOUNDED HARBOR SEAL WHISKER INSPIRED PIN GEOMETRIES
PREMIXED REACTING JET FLOW BEHAVIOR IN AN AXIALLY STAGED MODEL COMBUSTOR AT ELEVATED PRESSURE
Propellants and combustion / American Institute of Aeronautics and Astronautics ; Volume 1 of 2
Propellants and combustion / American Institute of Aeronautics and Astronautics ; Volume 2 of 2
Rechnerische Untersuchung des Schwingungsverhaltens eines hochtourigen Rotors
REDUCED-ORDER MODELING OF AEROELASTICITY IN EXTREME SPEED TURBOCHARGERS
Regelungstechnische Verfahren zur aktiven Minderung von Rotorschwingungen
Regression simulation of turbine engine performance/aircraft regression model
Research trends and opportunities in air breathing propulsion
Revolutionäre Arbeitsprozesse : REVAP : Abschlussbericht : Berichtszeitraum: 01.01.12-31.12.13
ROBUST, EFFICIENT AND ACCURATE MESH ADAPTATION FOR TURBOMACHINERY CFD SIMULATIONS