Team6-NASAGreenAviationChallenge

Team6-NASAGreenAviationChallenge - NASA Green Aviation...

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Click to edit Master subtitle style 8/7/11 NASA Green Aviation Challenge David Axel Virzi Marina Correia William Tejada
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8/7/11 The Challenge Design non-conventional aircraft to assist in the goals set forth in the NASA metrics below Noise reduction, reduced fuel consumption,
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8/7/11 Problem Statement Aerodynamic design of a 200 passenger aircraft for Drag reduction Reduced fuel consumption Lower acoustic signature Weight reduction Incorporation of co-flow jet on a morphing wing to assist in aforementioned requirements by
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8/7/11 Conventional Aircraft Tube design is not the most aerodynamically efficient design Design features several surfaces such as the vertical and horizontal stabilizers that increase the overall drag of the aircraft Passenger and cargo limitations – large aircraft such as the Boeing 747 and Airbus A380 feature tall designs that induce a lot of drag
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8/7/11 Airframe Design Comparison Type of Design Drag Coefficient Lift Coefficient
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This note was uploaded on 08/07/2011 for the course EML 4905 taught by Professor Staff during the Spring '08 term at FIU.

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Team6-NASAGreenAviationChallenge - NASA Green Aviation...

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