Synonyme wurden verwendet für:
Flugtriebwerk
Suche ohne Synonyme:
keywords:(Flugtriebwerk)
Brayton Cycle Analysis of the Effect of Wake Ingestion on Aircraft Range
Spectral Proper Orthogonal Decomposition Downstream of a Vortex Tube Separator Array
Computational Assessment of Non-Axisymmetric Separate-Jet Exhausts on Test Rig Configurations
Design Considerations of Non-Axisymmetric Exhausts for Large Civil Aero-Engines
Unsteady Analysis of Ground Vortex Ingestion with LBM-VLES
CFD SIMULATION OF AN INWARD-TURNING SUPERSONIC INLET UNSTART AT FLIGHT MACH NUMBER 1.7
AGGRESSIVELY-OFFSET INLET FLOW FACILITY DESIGN AND CHARACTERIZATION
Summary of the 5th Propulsion Aerodynamics Workshop: Inlet Cross-Flow Results
Some Design Considerations for Two-Dimensional, Mixed-Compression Inlets for Mach 2.5 to 3.5
Assessment of Engine Modelling on the Installed Aerodynamics of an Ultra-High Bypass Turbofan
CFD Modeling of Turbofan Intake Aerodynamics at Crosswind Conditions
Effect of Small Step on Aerodynamic Performance in the Transonic Inlet
Design Optimization of a Fan Blade Under Boundary Layer Ingestion Flow
A unified analytical approach for the acoustic conceptual design of fans of modern aero-engines
SIMULATIONS OF AN AIRFRAMF-INTEGRATED TWO-DIMENSIONAL SUPERSONIC INLET AT OFF-DESIGN CONDITIONS
FLOW DISTORTION COMPUTATIONAL MODELING AND DESIGN OPTIMIZATION FOR SUPERSONIC INLET
Überblick über neue Antriebssysteme und Technologien von Flugzeugen
BCFD Analysis for the 5th AIAA Propulsion Aerodynamics Workshop: Film Cooled Nozzle Results
PARAMETRIC STUDY OF INTERACTION BEHAVIOR OF LAMINAR JETS
Parametric Study of Interaction Behavior of Laminar Jets
Design of Short Intakes for Ultra-High Bypass Engines: Preliminary Exploration at Fixed Incidence
Propellants and combustion / American Institute of Aeronautics and Astronautics ; Volume 2 of 2
Untersuchung des Wärmeübergangs durch Einspritzkühlung für ein Höchstleistungsgetriebe
INVESTIGATION OF THE EFFECTS OF LOBE NUMBER AND CONFIGURATION ON MIXING PERFORMANCE IN LOBED MIXER
NEARFIELD ANISOTROPIC MESH ADAPTIVITY FOR THE THIRD AIAA SONIC BOOM WORKSHOP
Deep-Learning for Flow-Field Prediction of 3D Non-Axisymmetric Aero-Engine Nacelles
Design of a High-Speed Intake Distortion Simulator for Propulsion Integration Research