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October 4, 2010, 14:55
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Aerodynamic Analysis
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New Member
anonymous
Join Date: Sep 2010
Posts: 2
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I am tasked with performing an aerodynamic analysis for flow over the fuselage of an aircraft to evaluate the flow characteristics of two different designs.
The aircraft has a maximum speed of 308 knots and a maximum altitude of 35,000 feet. Does anyone know of any reference information on this type of analysis? thanks in advance |
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