Transcription of DESIGN OF AN AIRCRAFT MAIN WING SPAR
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DESIGN OF AN AIRCRAFT MAIN WING SPAR
DESIGN OF AN AIRCRAFT MAIN WING SPAR DESIGN PROJECT 2 Final Report AEE 471 | Davidson Assigned: October 24th, 2018 Due Date: November 16th, 2018 TYLER VARTABEDIAN TABLE OF CONTENTS TABLE OF CONTENTS2 BACKGROUND AND PROVIDED INFORMATION3 RESULTS8 SUMMARY8 CROSS SECTION 1 - X=120 (AT WALL)11 CROSS SECTION 2 - X=10812 CROSS SECTION 3 - X=9613 CROSS SECTION 4 - X=8414 CROSS SECTION 5 - X=7215 CROSS SECTION 6 - X=6016 CROSS SECTION 7 - X=4817 CROSS SECTION 8 - X=3618 CROSS SECTION 9 - X=2419 CROSS SECTION 10 - X=1220 CROSS SECTION 11 - X=0 (AT WING TIP)21 Fatigue: N/A21 STRESS CALCULATIONS and FACTORS OF SAFETY22 WEIGHT CALCULATION24 FATIGUE25 TIP DEFLECTION28 APPENDIX A: HAND CALCULATIONS30 APPENDIX B: TIP DEFLECTION CALCULATIONS31 APPENDIX C: SUPPORTING FIGURES32 APPENDIX D: SUPPORTING CODE33 Vartabedian - 2 BACKGROUND AND PROVIDED INFORMATION The goal of this projec
These allowables are taken from the allowables where an area is assumed to be less than 20 square inches, and the extruded beam has a thickness in-between 3.1 and 4.4 inches. Figure 1 - Geometry and Loading of Main Wing Spar ( A E E 471 P r oj e c t 2 Handout - …
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