Airfoil Method for Rotary Wing Analysis Using Modified Lift and Drag Equations
Airfoil Method for Rotary Wing Analysis Using Modified Lift and Drag Equations
- New search for: T. Kraeutner
- New search for: T. Kraeutner
This paper will demonstrate how to adapt fixed wing lift/drag equations to analyze rotary wings as airfoils. This Airfoil method is validated by analysis of eight radio controlled helicopters and quad-copters, which are flown at a hover for a known time duration.
Document information
Airfoil Method for Rotary Wing Analysis Using Modified Lift and Drag Equations
2021
89 pages
Report
No indication
English
Aerodynamics , Aeronautics , Aircraft , Aircrafts , Airfoils , Aspect ratio , Coefficients , Computer programs , Efficiency , Equations , Helicopters , Intervals , Models , Momentum , Motors , Power , Propellers , Reynolds number , Stabilization systems , Tail rotors
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