# HW1 - For flight conditions given in#1 above what is the...

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AAE 334, Fall 2011, Homework 1 Due Wednesday, August 24 at the beginning of class. Simple review problems. Show units throughout and work the problem in the system of units in which it is posed. 1. For a flow of air with density of 0.85 kilograms per cubic meter and speed of 60 meters per second, find the dynamic pressure in Pascals. 2. An airfoil with a 2 meter chord has a lift coefficient of 0.28.
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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.

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