Unformatted text preview: For flight conditions given in #1 above, what is the lift force per span generated by the airfoil? 3. For a flow of air with a dynamic pressure of 0.75 psi and density of 0.002 slug per cubic foot, find the air speed in feet per seconds. 4. An airfoil with a 6 foot chord generates a lift force per span of 90 pounds per foot. For flight conditions given in #3 above, what is the lift coefficient?...
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This note was uploaded on 02/21/2012 for the course AAE 334 taught by Professor Collicott during the Fall '09 term at Purdue.
- Fall '09