spl7c - Test rig: Force balance in 1 1 wind tunnel. Drag...

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Plain Vanilla Fuselage Drag Measurements 23 Mar 06 Lab 7 Lecture Notes C Plane Vanilla Drag Test Results Test article: Plane Vanilla fuselage, prop off.
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Unformatted text preview: Test rig: Force balance in 1 1 wind tunnel. Drag results: q (Pa) D (N) 5.47 0.0211 11.06 0.0411 20.79 0.0877 31.46 0.1243 1...
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This note was uploaded on 01/28/2012 for the course AERO 16.01 taught by Professor Markdrela during the Fall '05 term at MIT.

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