Header1200x385

× Welcome to the CPL Aerodynamics question and answer forum. Please feel free to post your questions but more importantly also suggest answers for your forum colleagues. Bob himself or one of the other tutors will get to your question as soon as we can.

Static Pressure

  • Afa
  • Topic Author

Afa created the topic: Static Pressure

What happen to static pressure on top and below of the aerofoil when angle of attack is increasing?
#1

Please Log in or Create an account to join the conversation.

  • John.Heddles
  • Offline
  • ATPL/consulting aero engineer
  • Posts: 891
  • Thank you received: 115

John.Heddles replied the topic: Static Pressure

Although the detail is a little more complex, as the angle of attack increases the overall static pressure over the upper surface decreases while that on the lower surface increases.

You will be familiar with the usual textbook pictures with arrows pointing away from the surfaces at right angles when the aerofoil is in a moving airflow. These show the magnitude of the static pressure as measured by what we call pressure tappings on the aerofoil's surface.

The difference between static pressure on the upper and lower surfaces is what provides lift, drag, and pitching forces on the wing.

Engineering specialist in aircraft performance and weight control.
#2
The following user(s) said Thank You: Afa

Please Log in or Create an account to join the conversation.

  • Afa
  • Topic Author

Afa replied the topic: Static Pressure

Thank you Sir.
#3

Please Log in or Create an account to join the conversation.

Time to create page: 0.085 seconds