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IND FLOW

AERODYNAMICS. L. TAF. C. L. RES RW. AoA. IND FLOW. D. ROT RW. AoA : angle measured between the resultant rw and the chord. CL : straight line intersecting the leading and trailing edges of the airfoil. TAF : resultant of Lift andDrag.

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IND FLOW

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  1. AERODYNAMICS L TAF C L RES RW AoA IND FLOW D ROT RW AoA: angle measured between the resultant rw and the chord. CL: straight line intersecting the leading and trailing edges of the airfoil. TAF: resultant of Lift andDrag. IND FLOW: flow drawn in as the flow induced by the vortex system of the rotor. RES RW: airflow from rotation that is modified by induced flow. ROT RW: airflow created by the rotation of the rotorblades. LIFT: is perpendicular to resultant relative wind. DRAG: is parallel to resultant relative wind and opposite thrust. 1) PROFILE: Frictional resistance of blade passing through the air. 2) INDUCED: drag induced by the production of aerodynamic force. 3) PARASITE: drag incurred from non-lifting components of the aircraft.

  2. AERODYNAMICS L TAF C L RES RW AoA IND FLOW D ROT RW _____: angle measured between the resultant rw and the chord. _____: straight line intersecting the leading and trailing edges of the airfoil. _____: resultant of Lift andDrag. _____: flow drawn in as the flow induced by the vortex system of the rotor. _____: airflow from rotation that is modified by induced flow. _____: airflow created by the rotation of the rotorblades. ______: is perpendicular to resultant relative wind. ______: is parallel to resultant relative wind and opposite thrust. 1) _______: Frictional resistance of blade passing through the air. 2) _______: drag induced by the production of aerodynamic force. 3) _______: drag incurred from non-lifting components of the aircraft.

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