Synonyms were used for:
Flugmechanik
Search without synonyms:
keywords:("Flugmechanik")
GPM Orbital Maintenance Planning and Operations in Low Solar Activity Environment
An Assessment of Aircraft Control via SISO Control Loops and Total Energy Control
Assessment of the Handling Qualities of Multirotor Configurations using Real Time Simulation
Aeroservoelastic Modeling of Body Freedom Flutter for Control System Design
Interpretation of Vehicle Tumbling Predictions from 6-DOF Entry and Descent Simulation
Aerodynamic Stability of the Dragonfly Aeroshell in the Transonic Dynamics Tunnel (Invited)
Influence of Electric Propulsion on Performance and Flight Mechanics of VTOL Aircraft
Design and Fabrication of the Boundary Layer Ingesting Tailcone System CRM-TCT Model in the NTF
AeroFusion: Data Fusion and Uncertainty Quantification for Entry Vehicles
Direct Numerical Simulation of A Turbulent Separation Bubble With Sweep
FUN3D Analyses in Support of the 5th Propulsion Aerodynamics Workshop - Nozzle Test Case
FUN3D Analyses in Support of the 5th Propulsion Aerodynamics Workshop (PAW5) - Inlet Test Case
Hydrocarbon Cold-Flow Simulation of LOX/LH2 Rocket Aerodynamics
Dragonfly Entry and Descent Flight Mechanics Modeling and Analysis
In search of data-driven improvements to RANS models applied to separated flows
Ablating Woven Thermal Protection System Materials Under High Shear Flow Conditions
Ongoing Aeroelastic Optimization Research at NASA LaRC, Aeroelasticity Branch
Nonlinear Development and Secondary Instability of Traveling Crossflow Vortices
Inside NASA’s X-57 Configuration - More than Just Electrifying an Airplane
Ongoing Subsonic Aeroelastic Optimization Research at NASA LaRC, Aeroelasticity Branch
Electrical Drive and Regeneration in General Aviation Flight with Propellers
HLPW-4/GMGW-3: Mesh Adaptation for RANS Technology Focus Group Workshop Summary
Design of a Crossflow Attenuated Natural Laminar Flow Flight Test Article
FUN3D Airload Predictions for the Full-Scale UH-60A Airloads Rotor in a Wind Tunnel
Development of the model deformation system at the National Transonic Facility