Calculating Lift

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Across
  1. 1. if you double the velocity of an aircraft it will do this to the lift
  2. 6. can't be controlled by a pilot without a change in position or altitude
  3. 7. are on the leading edge of larger and more complex aircraft that will allow the pilot to increase the surface area of a wing
  4. 10. an airfoil that has a higher coefficient of lift than a thin, symmetrical airfoil
  5. 12. in the lift formula is it what s stands for
  6. 13. in the lift formula is it what v stands for
  7. 14. in the lift formula is it what CL stands for
Down
  1. 2. the force the pulls the airplane into the sky
  2. 3. a type of airfoil where the upper and lower surfaces of the airfoil are identical
  3. 4. an imaginary line connecting the leading edge with the trailing edge of an airfoil
  4. 5. a type of airfoil where the upper surface is more curved
  5. 8. is what AOA stands for
  6. 9. in the lift formula is it what p stands for
  7. 11. can be deployed to change the shape of an airfoil to create more lift