DesignReview3_9_01

DesignReview3_9_01 - AAE 490T/590T March 9th 2001 PRESENTED...

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HYPERION  Design Review AAE 490T/590T March 9th, 2001 PRESENTED BY: John Castro Loren Garrison Chris Peters Jeff Rodrian Thomas Schmidt-Lange
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Outline Historical Database Parameter Selection Weight Determination Fixed Weights Weight Estimation Process Optimization Parameters Aerodynamics Structures Results and Final Aircraft Specifications Construction Methods Wing Structure Assembly Process Mold Making Fuselage Structure Concerns
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Historical Database Name Style Wing Area [in 2 ] Wingspan [in] AR Wing Wing Loading [oz/ft 2 ] Length [in] Weight [lbs] Topline 97 Pattern 1040 75 5.41 22.15 78.5 9 Caprise Pattern 1060 76.8 5.56 23.26 78.5 9.7 Alliance Pattern 1062 76 5.49 22.68 78.5 9.46 Topline 1 Pattern 961 73 5.52 24.55 74.8 9.24 EXTREM Pattern 1101 76 5.19 21.44 78.3 9.24 Desafio II Pattern 840 68.8 5.64 27.43 65 9 Desire Pattern 940 66 4.63 23.90 69 8.75 Dr. Jeckyll Pattern 970 76 5.95 23.75 78 9 Fascination Pattern 1036 78 5.87 24.46 77 10 Omen Pattern 1150 78.5 5.36 22.04 78.5 10 Extra 300S IMAC 895 70 5.47 28.96 61 10.25 CAP 231 IMAC 900 75 6.25 28.16 66 10 Edge 540 IMAC 930 73 5.73 26.01 64 9.5 Wild Beat Pattern 1077 76 5.36 22.68 77.75 9.6 AVERAGE 997.28 74.14 5.53 24.39 73.21 9.48 HYPERION Pattern 1002 75 5.62 25 78 10 AR HT = 4.0 AR VT = 0.8 λ W = 0.45 Λ W C/4 = 0 deg
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Fixed Weight Breakdown Weight [oz] Weight Fraction (%) 68.4 18.2 13.4 7.1 100.0 C.G. of Fixed Fuselage Components VT 149.8 34.2 74.4
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Tail Sizing and Placement Matlab Optimization Code Uses fmincon Matlab function Objective
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DesignReview3_9_01 - AAE 490T/590T March 9th 2001 PRESENTED...

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