Helicopter Lessons: Transverse Flow Effect
Presenter: Jacob
Series: Helicopter Lessons in 10 Minutes or Less
Introduction
- Feedback & Interaction: Encourages viewers to like, comment, and provide feedback on videos.
- Topic of Discussion: Transverse Flow Effect in helicopters.
What is Transverse Flow Effect?
- Definition: The right rolling motion and slight vibrations occurring as a helicopter accelerates into forward flight.
- Flow Transition: Transition of airflow from vertical (stationary hover) to horizontal (forward flight).
- Speed Range: Occurs between 10 to 20 knots of airspeed.
Detailed Explanation
- Airflow Dynamics:
- Stationary Hover: Airflow is vertical through rotor system.
- Forward Flight: Airflow becomes horizontal, affecting front and rear parts of rotor disc differently.
- Front Half: More horizontal airflow, more lift.
- Aft Half: More vertical airflow, less lift.
Airfoil Analysis
Resulting Motion and Correction
- Lift Distribution: More lift on front half than aft half.
- Gyroscopic Precession: Phenomenon causes effects to manifest 90 degrees later in the rotor disc.
- Compensation: Use of left cyclic to counteract right roll.
Practical Example
-
Takeoff Scenario:
- Helicopter starts takeoff.
- Experiences right roll pushing it to the right of the lane.
- Pilot corrects back to center or continues forward.
-
Approach Scenario:
- Between 10 to 20 knots, right roll pushes to side.
- Correction required to maintain lane.
- Potential for vibrations due to drag variance.
Conclusion
- Transverse Flow Summary:
- Right rolling motion between 10-20 knots.
- Simple to compensate with left cyclic.
- Closing Remarks:
- Thanks viewers, encourages likes, subscribes, and feedback.
- Jacob signs off from Helicopter Lessons.