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Flugtriebwerk
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Time-Varying Operating Condition–Based Prediction of the Remaining Useful Life for Aeroengine
Fuel consumption estimation for jet aircraft: a mathematical model development
Exploring the possibilities of using bio-additives in military aviation fuels
Optimization of Lift-Plus-Cruise Vertical Take-Off and Landing Aircraft with Electrified Propulsion
Review of Contemporary Methods for Reliability Analysis in Aircraft Components
Evaluating an Additive Manufactured Acoustic Metamaterial Using the Advanced Noise Control Fan
Shock-Induced Separation and Control in a 4.32-Aspect-Ratio Test Section
Review of the hybrid gas - electric aircraft propulsion systems versus alternative systems
Event-Triggered Model Predictive Control for Aero-Engine Transient-State Tracking Problems
Two-Way Blade Modeling Method for Structural Redesign of Compressor Blades
Mistuning Identification of Blisks Using Mass Detuning and Influence Coefficients
Experimental Investigation on Ice Accretion Upon Ice Particle Impacting onto Heated Surface
Stabilisation of Hydrodynamic Instabilities by Critical Layers in Acoustic Lining Boundary Layers
Instability of Rotating-Cone Boundary Layer in Axial Inflow: Effect of Cone Angle
Interacting Linear Modes in the Turbulent Flow of an Industrial Swirled Combustor
Impact of Airframe–Propulsion System Modeling Strategies on Key Structural Performance Metrics
A novel full-electric aircraft propulsion based on the DEA compressor
Environmental and enviroeconomic impacts of COVID-19 pandemic on commercial flights
Augmenting effectiveness of geared turbofan engines by dual stage radial blisks
Convolution for Haystacking in Turbulence-Ingesting Rotor Noise
Optimal Sensor Placement for Azimuthal Acoustic Modes in Cylindrical Ducts
Design and Sizing of an Electrified Lift-Plus-Cruise Ducted Fan Aircraft
Benefits and Challenges of the Inside-Out Ceramic Turbine: An Experimental Assessment
Low-Thrust Solid Rocket Motors for Small, Fast Aircraft Propulsion: Design and Development
Low-Noise Blade Design Optimization for a Transonic Fan Using Adjoint-Based Approach
Hurst Exponents for Intra- and Intercycle Thermoacoustic Oscillations
Comparison of Electrified Aircraft Propulsion Drive Systems with Different Electric Motor Topologies
System Identification for Propellers at High Incidence Angles
Evaluation of piston engine modes and configurations in composite cycle engine architectures
Evaluation of piston engine modes and configurations in composite cycle engine architectures
Numerical modelling of turbofan engine deterioration as a factor in the airlines fuel conservation
Aerodynamic Analysis and Design of a Rim-Driven Fan for Fast Flight
Sound Production due to Swirl–Nozzle Interaction: Model-Based Analysis of Experiments
Continuous Open Access Special Issue "Aircraft Design": Number 2/2020
NASA electrified aircraft propulsion efforts
Confidence interval prediction of ANN estimated LPT parameters
Introduction to the Special Issue on Advances in Bio-Inspired Propulsion
Magnetization and Losses for an Improved Architecture of Trapped-Flux Superconducting Rotor