| A | B | C | D | E | F | G | H | I | J | K | L | |
|---|---|---|---|---|---|---|---|---|---|---|---|---|
1 | Scale | Density slug/ft3 | Density slug/ft3 | Density slug/ft3 | MaxGTOW | Thrust | Flat Plate | Convert | Convert | Convert | Convert | Convert |
2 | Height (km) | (MSL) | 35.00 | 60.00 | (lbs) | fwd (lbs) | Cd | km/h to kts | kgs to lbs | HP to lb | m to ft | m² to ft² |
3 | 15.9 | 0.1300014622 | 0.01438646504 | 0.002986077917 | 76,345 | 139,382 | 1.35 | 0.5405405405 | 2.2046 | 167.64 | 3.2808 | 10.7636 |
4 | ||||||||||||
5 | Pitch Section | Arm Y Dh (m) | Wing Arm m | Arm (ft) | ||||||||
6 | Pitching Drag | 4.882029 | -2.440206 | 16.01696074 | ||||||||
7 | ||||||||||||
8 | Yaw Section | Arm Y Dv (m) | Wing Arm m | Critical | Arm (ft) | Rudder m² | Rudder ft² | Remain ft² | Torque lb-m | Torque lb-ft | Required | |
9 | Yawing Drag | 2.787865 | 17.567850 | 5.054167543 | 9.146427492 | 6.922942 | 74.5161 | -74.5161 | 92,254 | 302,668 | 33,091 | |
10 | ||||||||||||
11 | Roll Section | Arm X (m) | Wing Arm m | |||||||||
12 | Rolling Drag | 0.232895 | 17.567850 | |||||||||
13 | ||||||||||||
14 | Lift Section | Area m² | Area ft² | Cl (T/O) | Cx (T/O) | Lift | at T/O | Cl (mcp) | Cx (mcp) | Lift | at mcp | |
15 | Wing VCl | 141.26598 | 1520.54 | 0.350000 | 34.592613 | 689,885 | pounds | 0.001152 | 0.012595 | 76,345 | pounds | |
16 | H-Stabilizer | 0.00 | 0.00 | 0.059648 | 0.000000 | 0 | pounds | -0.375000 | 0.000000 | 0 | pounds | |
17 | V-Stabilizer | 0.00 | 0.00 | n/a | n/a | n/a | n/a | n/a | n/a | |||
18 | ||||||||||||
19 | Drag Section | Area m² | Area ft² | Cx (T/O) | Drag | at T/O | Cx (mcp) | Drag | at mcp | |||
20 | Frontal Drag | Total | 38.340908 | 412.688062 | 0.364097 | 29,502 | pounds | 0.022995 | 139,382 | pounds | ||
21 | ||||||||||||
22 | FWD/BACK | UP/DOWN | LFT/RIGHT | |||||||||
23 | Arm Y (m) | Arm Z (m) | Arm X (m) | |||||||||
24 | Left Engine Intake | Frontal | 1.638330 | 17.63 | 1.280000 | 1.467199 | n/a | 0.092357 | -1.540529 | |||
25 | Landing Struts | Frontal | 6.543327 | 70.43 | 0.500000 | 2.289003 | n/a | -0.243516 | -0.002317 | |||
26 | Flat Plate Front | Frontal | 31.797581 | 342.26 | 0.045000 | 1.001116 | n/a | -0.010901 | 0.003198 | |||
27 | Flat Plate Bottom | Plan | 187.309021 | 2016.13 | 1.350000 | 176.917265 | -4.670942 | n/a | 0.000296 | |||
28 | Flat Plate Sides | Profile | 100.137909 | 1077.85 | 1.350000 | 94.582337 | -2.396915 | -0.022551 | n/a | |||
29 | Landing Struts | Profile | 11.618149 | 125.05 | 1.350000 | 10.973583 | -0.413568 | -0.163337 | n/a | |||
30 | ||||||||||||
31 | Airfoils | Options | Effective | YZ Radian | Cl (Max) | Cd (Max) | AOI | Cl (T/O) | Cd (T/O) | AOA | Cl mcp | Cd mcp |
32 | NACA0015 | NACA | 95.7% | 0.294001 | 0.7189 | 1.3500 | +0.000° | 0.350000 | 0.004250 | -3.000° | 0.001152 | 0.006000 |
33 | w/ Winglets | 0% | 95.7% | 0.294001 | 0.7189 | 1.3500 | +0.000° | 0.350000 | 0.004250 | -3.000° | 0.001152 | 0.006000 |
34 | ||||||||||||
35 | ||||||||||||
36 | ||||||||||||
37 | ||||||||||||
38 | ||||||||||||
39 | ||||||||||||
40 | Airfoils | Options | Cl (Max) | Cd (Max) | AOI | Cl (T/O) | Cd (T/O) | AOA | Cl mcp | Cd mcp | ||
41 | 63A010 | NACA | 0.8400 | 1.3500 | 2.292° | 0.059648 | 0.005500 | -0.708° | -0.375000 | 0.006000 | ||
42 | ||||||||||||
43 | VCL m² | HCL m² | Qty. | VCL ft² | HCL ft² | MAC m | Yaw Arm | Pitch Arm | Roll Arm | |||
44 | Tail Shroud | 96.0 | 1 | 1033.3 | 0.0 | 12.0 | 21.7 | 6.4 | 21.3 | |||
45 | Tail Fin | 42.0 | 2 | 904.1 | 0.0 | ??? | 13.3 | 8.3 | 10.8 | |||
46 | ||||||||||||
47 | Engines | Area m² | Qty. | Z Area m² | Cd | Power Ea. | XZ Radian | XZ DCM m | Yaw Arm | YZ Radian | YZ DCM m | Pitch Arm |
48 | Critical Engine | 3.3 | 2 | 6.7 | 16.18418 | 50.000% | 1.0338856 | 4.1 | 3.48922 | 0.158412 | 12.5 | 1.97753 |
49 | Tail Engine | 3.3 | 0 | 0.0 | 0.00000 | 50.348% | 0.0000000 | 0.0 | 0.00000 | 0.106246 | 37.7 | 3.99973 |
50 | ||||||||||||
51 | Velocity | (fps) | (m/s) | (km/s) | Indicated kms | (km/h) | (kts) | KIAS | Legend | |||
52 | Vs1 (MSL) | 98.536 | 30 | 0.030 | 0.010 | 108 | 58 | 19 | CHECK | |||
53 | Vmc (MSL) | 271.101 | 83 | 0.083 | 0.027 | 297 | 161 | 53 | OK | Descriptor | ||
54 | Vr (MSL) | 141.220 | 43 | 0.043 | 0.014 | 155 | 84 | 28 | Vmc+5%:Vr | Makeship | ||
55 | Published Vr | 284.656 | 87 | 0.087 | 0.029 | 312 | 169 | 56 | OK | Provided | ||
56 | V2 (MSL) | 298.211 | 91 | 0.091 | 0.030 | 327 | 177 | 59 | Viewscreen | |||
57 | Va (MSL) | 155.800 | 47 | 0.047 | 0.016 | 171 | 92 | 31 | Mach | OK | Calculated | |
58 | Vc (MSL) | 618.720 | 189 | 0.189 | 0.063 | 679 | 367 | 122 | 0.45 | OK | Constant | |
59 | Vc (Altitude) | 2461.977 | 750 | 0.750 | 0.114 | 2702 | 1460 | 221 | 2.83 | OK | ||
60 | Vne (Altitude) | 2769.724259 | 844 | 0.844 | 0.128 | 3039 | 1643 | 249 | 3.18 | OK | ||
61 | Vd (Altitude) | 3077.471399 | 938 | 0.938 | 0.142 | 3377 | 1825 | 277 | 3.54 | OK | ||
62 | Mach (MSL) | 1,387.778 | 423 | 0.423 | 0.141 | 1523 | 823 | 274 | 1.00 | |||
63 | Mach (Altitude) | 869.700 | 265 | 0.265 | 0.040 | 954 | 516 | 78 | 1.00 | |||
64 | ||||||||||||
65 | No Vs0 since we don't have flaps | |||||||||||
66 | We are still hiding a flight control calcuation issue | |||||||||||
67 | Never knew these were TAS not IAS values... V-speeds are always IAS so WTF was my teacher teaching us! | |||||||||||
68 | Vs1 at altitude (60km) was around 43 | |||||||||||
69 | ||||||||||||
70 | Structural | Category | Positive J | Positive J | Positive J | Positive J | Positive J | Negative J | Negative J | Negative J | Negative J | |
71 | Limits | Lower G | Lower lbs | Ultimate G | Ultimate lbs | Range lbs | Lower G | Lower lbs | Ultimate G | Ultimate lbs | ||
72 | Wings | Transport | 2.5 | 3.75 | -1 | -1.5 | ||||||
73 | ||||||||||||
74 | ||||||||||||
75 | Thermodynamics | Crit Sfc Tmp | 700 | K | ||||||||
76 | Absorption | Emission | ||||||||||
77 | 46687.72367 | 469764.4221 |