Synonyme wurden verwendet für:
Flugtriebwerk
Suche ohne Synonyme:
keywords:(Flugtriebwerk)
Comprehensive Validation of Skeletal Mechanism for Turbulent Premixed Methane–Air Flame Simulations
Markov Nonlinear System Estimation for Engine Performance Tracking
Modeling of crack growth with dwell time for aero-engine spectra loadings in a ni-based superalloy
Two-Phase Flow Pressure Drop in Corrugated Tubes Used in an Aero-engine Oil System
Evaluation of piston engine modes and configurations in composite cycle engine architectures
Numerical Determination of Contact Forces in Radial Roller Bearings with Flexible Rings
Microcooling Channel Effect on a Monopropellant Microelectromechanical System Thruster Performance
Effects of Water-Vapor Propellant on Electrodeless Thruster Performance
Robustness of a Turbine Endwall Film Cooling Design to Swirling Combustor Inflow
Robustness of a Turbine Endwall Film Cooling Design to Swirling Combustor Inflow
Development of High-Frequency Pulse Detonation Combustor Without Purging Material
Development of High-Frequency Pulse Detonation Combustor Without Purging Material
Effects of Tabbed-Nozzle on Pumping Performance of Incompressible Short Mixer–Ejector
Effects of Tabbed-Nozzle on Pumping Performance of Incompressible Short Mixer–Ejector
Comparison Between Excited Hydroxyl Radical and Blue Radiation from Hydrogen Rocket Combustion
Comparison Between Excited Hydroxyl Radical and Blue Radiation from Hydrogen Rocket Combustion
Effects of Recess on the Self-Pulsation Characteristics of Liquid-Centered Swirl Coaxial Injectors
Lanthanum Hexaaluminate Catalyst Support in a Hydrogen Peroxide Thruster
Lanthanum Hexaaluminate Catalyst Support in a Hydrogen Peroxide Thruster
Numerical Simulations of Mixing Enhancement in Subsonic Jet Using High-Momentum Synthetic Jets
Blade-Row Interaction Effects on Unsteady Stator Loading in an Embedded Compressor Stage
Blade-Row Interaction Effects on Unsteady Stator Loading in an Embedded Compressor Stage
Stall-Warning Approach Based on Aeroacoustic Principle
Stall-Warning Approach Based on Aeroacoustic Principle