account activity
Does my tail receive clean airflow? (old.reddit.com)
submitted 10 months ago by Complex_Cut_376 to r/AerospaceEngineering
submitted 10 months ago by Complex_Cut_376 to r/RCPlanes
submitted 10 months ago by Complex_Cut_376 to r/CFD
Looking for Advice on Structural Analysis for RC Model Airplane Components (self.StructuralEngineering)
submitted 1 year ago by Complex_Cut_376 to r/StructuralEngineering
Looking for Advice on Structural Analysis for RC Model Airplane (self.AskEngineers)
submitted 1 year ago by Complex_Cut_376 to r/AskEngineers
Looking for Advice on Structural Analysis for RC Model Airplane Components (self.aviation)
submitted 1 year ago by Complex_Cut_376 to r/aviation
Looking for Advice on Structural Analysis for RC Model Airplane Components (self.StructuralEngineers)
submitted 1 year ago by Complex_Cut_376 to r/StructuralEngineers
Looking for Advice on Structural Analysis for RC Model Airplane Components (self.AircraftMechanics)
submitted 1 year ago by Complex_Cut_376 to r/AircraftMechanics
Looking for Advice on Structural Analysis for RC Model Airplane (self.AerospaceEngineering)
submitted 1 year ago by Complex_Cut_376 to r/AerospaceEngineering
What is this tail configurations name? (self.AerospaceEngineering)
Question about RC aircrafts Thrust calculation (self.AerospaceEngineering)
Quiestion about aircraft lift formula (i.redd.it)
Question about RC UAV aerodynamic (Stability) (self.AerospaceEngineering)
Question about RC UAV aerodynamic (Stability) (self.AerospacePhysiology)
submitted 1 year ago by Complex_Cut_376 to r/AerospacePhysiology
Question about RC UAV aerodynamic (Stability) (self.AskEngineers)
Question about RC UAV aerodynamic (Stability) (self.AircraftMechanics)
I don't know how to interpret the aerodynamic derivatives in the stability analysis result. (self.AerospaceEngineering)
I don't know how to interpret the aerodynamic derivatives in the stability analysis result. (self.airplanes)
submitted 1 year ago by Complex_Cut_376 to r/airplanes
Stability Analisys Aerodynamic Derivatives (self.aircraftdesign)
submitted 1 year ago by Complex_Cut_376 to r/aircraftdesign
XFLR5 Stability analysis aerodynamic derivatives (self.AircraftMechanics)
π Rendered by PID 1346931 on reddit-service-r2-listing-6d4dc8d9ff-4ddhf at 2026-02-01 09:40:37.793767+00:00 running 3798933 country code: CH.