The design report

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Appendix 7 Appendix A – AVL files iSpy 0.0 Mach 0 0 0.0 iYsym iZsym Zsym 0.568985832 0.260 2.3 Sref Cref Bref 0.065 0.0 0.0 Xref Yref Zref 0.04308444 CDo #============================================= SURFACE Wing 10 1.0 30 -2.0 YDUPLICATE 0.00 ANGLE 1.0000 SCALE 1.0 1.0 1.0 TRANSLATE 0.0 0.0 0.0 #---------------------------------- # Xle Yle Zle chord angle Nspan Sspace SECTION 0.0 0.0 0.0 0.260 0.0 10 -2.0 AFIL NACA4415.dat #---------------------------------- # Xle Yle Zle chord angle Nspan Sspace SECTION 0.0 0.89 0.0 0.260 0.0 10 -2.0 AFIL NACA4415.dat #---------------------------------- # Xle Yle Zle chord angle Nspan Sspace SECTION 0.259 1.15 0.0 0.001 0.0 10 -2.0 AFIL NACA4415.dat #============================================= SURFACE Horizontal tail 10 1.0 YDUPLICATE 0.00000 ANGLE 0.000 SCALE 1.0 1.0 1.0 TRANSLATE 0.760 0.00000 0.00 #--------------------------- SECTION
0.000 0.00000 0.00000 0.180 0.000 10 0 AFIL MM010.dat #--------------------------- SECTION 0.000 0.365 0.00000 0.180 0.000 10 0 AFIL MM010.dat #============================================= SURFACE Vertical tail 14 1.0 YDUPLICATE 0.0 SCALE 1.0 1.0 1.0 TRANSLATE 0.78400 0.00000 0.00000 #--------------------------- SECTION 0.00 0.38400 0.0000 0.24000 0.000 10 1.5 #--------------------------- SECTION 0.096 0.38400 0.188856 0.144 0.000 10 0.5 # #============================================= BODY Fuse 12 1.0 # TRANSLATE -0.450 -0.384 0.0 # BFIL fuse.dat #============================================= # BODY Pod 12 1.0 # TRANSLATE -0.150 0.0 0.0 # BFIL pod.dat #============================================= # BODY Fuse 12 1.0 #
Page 1 and 2:
EP-UAV Project 2009 iSpy Kate Rietd
Page 3 and 4:
Preliminary and Detailed Design 4 S
Page 5 and 6:
Executive Summary 1 iSpy is a twin
Page 7 and 8:
Design Requirements and Objectives
Page 9 and 10:
Initial Sizing 3.1.2 Estimating air
Page 11 and 12:
Airfoil design 3.1.4 Wing: Before t
Page 13 and 14:
Tail: A symmetric airfoil with a th
Page 15:
Empennage design 3.1.6 The dimensio
Page 19 and 20: Pod Layout 3.1.9 The pod of the air
Page 21: Weight estimation and Centre of Gra
Page 26 and 27: Figure 3.2.303 - Stability axis der
Page 30 and 31: CAD definition of the concept 3.2.5
Page 32 and 33: Figure 3.2.505: The vertical tail F
Page 34 and 35: Preliminary and Detailed Design 4 S
Page 36 and 37: Figure 4.1.109 Figure 4.1.110 The c
Page 38 and 39: Material type was chosen for each c
Page 40 and 41: The nose section of the fuselage co
Page 42 and 43: This part of the fuselage is the mo
Page 44 and 45: Empennage structure 4.1.3 Prelimina
Page 46 and 47: An ‘L’ shaped support was also
Page 48 and 49: Landing gear 4.1.5 Initial stages o
Page 50 and 51: Pod Structure 4.1.7 Figure 4.1.701-
Page 52 and 53: Fuselage fabrication 5.2 Since ther
Page 54 and 55: The servo holder plates in front of
Page 56 and 57: Landing gear fabrication 5.5 The de
Page 58 and 59: Fabrication of Pod 5.6 Like the fus
Page 60 and 61: Control surface fabrication 5.9 Ail
Page 62 and 63: Note: The weights taken after fabri
Page 64 and 65: It was here that the first problem
Page 66 and 67: Flight Test 6.2 The flight test aim
Page 70 and 71: TRANSLATE -0.450 0.384 0.00 # BFIL
Page 72 and 73: CLARK YM-15 - Re = 250000 Alfa Cl C
Page 74 and 75: Appendix C - Preparation of materia
Page 76 and 77: Appendix D - Control surface sizing
Page 82 and 83: Conceptual Design Preliminary Desig
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The design report

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