ABCDEFGHIJKLMNOPQRSTUVWXYZ
1
Wing Name: Enzo3 XXS15/2/2024
Calcul Vitesse McCready moyenne
Extra drag loss
2
Voile et sellete de competitionG9,81m/s-2Tz2,5m/s(avg Lift)Glide loss0,000
points in glide
3
Total Weight in Flight9092,8
cinematic viscosity
1,45E-05Dz-0,5m/s(avg sink)
McCready average speed
0,00km/h
4
Height over sea level1000m [7]density1,11kg/m3Bx0km/h
Face wind < 0
Time loss on a 1.5h task
0,0minutes
5
Flat Aera19,150m2flat span12,06m
Point loss per task
0points
6
Flat Aspect Ratio7,600projecte span9,7m
point loss per competition
0points
7
Flat Ratio (Sproj/S)0,847line scale Maverage chord1,587mLegend:
km loss on a 10h XC flight
0km
8
Line drag aera SCx0,1490,149projected span16,22m2
Input taken from the wing
9
Pilot and Harness drag aera SCx0,114m2wing load4,7kg/m20,4600
Input for polar table and McCready
10
extra drag SCx0,000m²
projected wing load
5,5kg/m22%
intermediate calculations
11
Average Profile thickness0,167%
proj Aspect ratio
5,81,7Main output
12
profile drag coef Cx00,0120,34
13
add Cd by rugosity0,0012m
14
Oswald Efficiency0,94
Lift Curve Slope
0,062Cl / °
15
reference speed (Variable Area)15m/s
reference speed (Variable area)
54,0km/h
optimum glide ratio ( variable area)
10,57
optimum aera ( varibale area)
15,3m2
16
Max Ground Glide Ratio calculation :
Opt speed40,4km/hmax glide12,23Opt LiftCoef0,777
17
18
Polar calculation with Extra Dragwith brake onhand offwith speed bar
19
angle of attack in 2D profile (°) ref zeroLift12,3438,5866,0114,8304,0793,547
20
angle of attack in finite AR wing18,40812,8058,9647,2036,0825,290
21
Cz XFLR5 2D1,150,800,560,450,380,33
22
Cz ref wing aera0,970,680,470,3810,320,28
23
SCz ref wing aera18,65312,9769,0837,2996,1645,361
24
SCx induit1,1280,5460,2680,1730,1230,093
25
SCx profile0,3600,2530,2530,2530,2530,253
26
TOTAL SCx1,7511,0620,7830,6890,6390,609
27
Total SCforce18,73513,0199,1177,3316,1975,395
28
Induced Drag (% total)64%51%34%25%19%15%
29
Profile Drag (% total)21%24%32%37%40%42%
30
Lines Drag (% total)9%14%19%22%23%24%
31
Harness+Pilot Drag (% total)7%11%15%17%18%19%
32
ExtraDrag SCx0%0%0%0%0%0%
33
Speed on trajectory (m/s)920%1104%1319%1471%1600%1715%
34
Horizontal Speed (m/s)916%1100%1314%1465%1592%1704%
35
Horizontal Speed(km/h)33,039,6147,3152,757,3061,34
36
Sink Rate (m/s)-0,86-0,90-1,13-1,38-1,65-1,94
37
Air Glide Ratio10,712,211,610,69,68,8
38
Ground Glide Ratio10,712,211,610,69,68,8
39
Average MacCready Speed (km/h)18,021,423,724,624,824,7
40
Reynolds number on average Chord1,01E+061,21E+061,44E+061,61E+061,75E+061,88E+06
41
angle finesse5,364,684,935,395,926,48
42
angle chord/horizon13,08,14,01,80,2-1,2
43
44
Polar calculation (without ExtraDrag)with brake onhand offwith speed bar
45
angle of attack in 2D profile (°) ref zeroLift12,3438,5866,0114,8304,0793,562
46
angle of attack in finite AR wing18,40812,8058,9647,2036,0825,313
47
Cz (ref wing aera)1,150,800,560,450,380,33
48
0,970,680,470,3810,320,28
49
SCz18,65312,9769,0837,2996,1645,383
50
SCx induit1,1280,5460,2680,1730,1230,094
51
SCx profile0,3600,2530,2530,2530,2530,253
52
TOTAL SCx (No extra drag !)1,7511,0620,7830,6890,6390,610
53
Total SCforce18,73513,0199,1177,3316,1975,418
54
Induced Drag (% total)64%51%34%25%19%15%
55
Profile Drag (% total)21%24%32%37%40%41%
56
Lines Drag (% total)9%14%19%22%23%24%
57
Harness+Pilot Drag (% total)7%11%15%17%18%19%
58
Speed on trajectory (m/s)920%1104%1319%1471%1600%1711%
59
Horizontal Speed (m/s)916%1100%1314%1465%1592%1700%
60
Horizontal Speed(km/h)33,039,6147,3152,757,3061,21
61
Sink Rate (m/s)-0,86-0,90-1,13-1,38-1,65-1,93
62
Air Glide Ratio10,712,211,610,69,68,8
63
Ground Glide Ratio10,712,211,610,69,68,8
64
Average MacCready Speed (km/h)18,021,423,724,624,824,7
65
Reynolds number on average Chord1,01E+061,21E+061,44E+061,61E+061,75E+061,87E+06
66
67
68
69
absolute drags
70
Induced Drag (daN)533726211815
71
Profile Drag (daN)171724303641
72
Lines Drag (daN)71014182124
73
Harness+Pilot Drag (daN)5811141619
74
Extra Drag (daN)000000
75
76
77
78
79
80
81
82
83
84
85
86
87
88
89
90
91
92
93
94
95
96
97
98
99
100