Design Name: | P-5 |
Designer: | Makarov A.V. |
Design Date: | 05.02.2007 |
File Name: | C:\Program Files\AirplanePDQ\P-5_2.dwg |
Parameter | SI Units | User Units |
---|---|---|
Ref Position X | 4.992 m | 4.992 m |
Y | 0.0 m | 0.0 m |
Z | 0.008111 m | 0.008111 m |
Model | VMKB M-14P(360 HP) | |
Type | piston | |
Max Power | 2.685e+05 watts | 268.5 kW |
Width | 0.9855 m | 0.9855 m |
Length | 0.9246 m | 0.9246 m |
Height | 0.9855 m | 0.9855 m |
Parameter | SI Units | User Units |
---|---|---|
Ref Position X | 5.019 m | 5.019 m |
Y | 0.0 m | 0.0 m |
Z | 0.003098 m | 0.003098 m |
Diameter | 2. m | 2. m |
Number of Blades | 3 | |
Mean Chord | 0.1155 m | 0.1155 m |
Mean Pitch | 1.342 m | 1.342 m |
Propeller Type | Constant Speed |
Parameter | SI Units | User Units |
---|---|---|
Ref Position X | 3.289 m | 3.289 m |
Y | 0.0 m | 0.0 m |
Z | -0.4567 m | -0.4567 m |
Aerodynamic Center Position | 4.06 m | 4.06 m |
Ref Area | 9.938 m^2 | 9.938 m^2 |
Exposed Area | 8.401 m^2 | 8.401 m^2 |
Wetted Area | 20.28 m^2 | 20.28 m^2 |
Span | 8.633 m | 8.633 m |
Fuselage Cutout | 0.4788 m | 0.4788 m |
Mean Aerodynamic Chord | 1.157 m | 1.157 m |
Aspect Ratio | 7.499 | |
Root Airfoil Section | 2412 | |
Root Airfoil Thickness | 12 | |
Tip Airfoil Section | 2412 | |
Tip Airfoil Thickness | 12 | |
Root Chord | 1.659 m | 1.659 m |
Tip Chord | 0.6435 m | 0.6435 m |
Taper Ratio | 0.3879 | |
Root Incidence | 0.05236 rad | 3. deg |
Twist | 0.0 rad | 0.0 deg |
Dihedral | 0.05236 rad | 3. deg |
Sweep (1/4 c) | 0.3488 rad | 19.99 deg |
Control Surface | Flaps | |
% Span | 30.42 | |
Mean % Chord | 18.42 | |
Inboard Edge (% semi span) | 22.94 | |
Control Area | 0.6151 m^2 | 0.6151 m^2 |
Affected Wing Area | 3.339 m^2 | 3.339 m^2 |
Control Surface | Ailerons | |
% Span | 44.57 | |
Mean % Chord | 4.898 | |
Inboard Edge (% semi span) | 53.76 | |
Control Area | 0.1671 m^2 | 0.1671 m^2 |
Affected Wing Area | 3.411 m^2 | 3.411 m^2 |
Parameter | SI Units | User Units |
---|---|---|
Ref Position X | 0.7724 m | 0.7724 m |
Y | 0.0 m | 0.0 m |
Z | -0.3058 m | -0.3058 m |
Aerodynamic Center Position | 0.7703 m | 0.7703 m |
Ref Area | 2. m^2 | 2. m^2 |
Exposed Area | 1.77 m^2 | 1.77 m^2 |
Wetted Area | 4.082 m^2 | 4.082 m^2 |
Span | 4. m | 4. m |
Fuselage Cutout | 0.23 m | 0.23 m |
Mean Aerodynamic Chord | 0.5 m | 0.5 m |
Aspect Ratio | 8. | |
Root Airfoil Section | 2412 | |
Root Airfoil Thickness | 12 | |
Tip Airfoil Section | 2412 | |
Tip Airfoil Thickness | 12 | |
Root Chord | 0.5 m | 0.5 m |
Tip Chord | 0.5 m | 0.5 m |
Taper Ratio | 1. | |
Root Incidence | 0.0 rad | 0.0 deg |
Twist | 0.0 rad | 0.0 deg |
Dihedral | 0.0 rad | 0.0 deg |
Sweep (1/4 c) | 0.0 rad | 0.0 deg |
Control Surface | Elevator | |
% Span | 81.83 | |
Mean % Chord | 39.73 | |
Inboard Edge (% semi span) | 16.9 | |
Control Area | 0.6503 m^2 | 0.6503 m^2 |
Affected Wing Area | 1.637 m^2 | 1.637 m^2 |
Parameter | SI Units | User Units |
---|---|---|
Ref Position X | 5.175 m | 5.175 m |
Y | -4.318 m | -4.318 m |
Z | -0.2542 m | -0.2542 m |
Aerodynamic Center Position | 5.466 m | 5.466 m |
Ref Area | 1.21 m^2 | 1.21 m^2 |
Exposed Area | 1.21 m^2 | 1.21 m^2 |
Wetted Area | 2.449 m^2 | 2.449 m^2 |
Span | 1.401 m | 1.401 m |
Fuselage Cutout | 0.0 m | 0.0 m |
Mean Aerodynamic Chord | 0.4495 m | 0.4495 m |
Aspect Ratio | 1.622 | |
Root Airfoil Section | 0009 | |
Root Airfoil Thickness | 9 | |
Tip Airfoil Section | 0009 | |
Tip Airfoil Thickness | 9 | |
Root Chord | 0.5828 m | 0.5828 m |
Tip Chord | 0.281 m | 0.281 m |
Taper Ratio | 0.4821 | |
Root Incidence | 0.0 rad | 0.0 deg |
Twist | 0.0 rad | 0.0 deg |
Dihedral | 1.728 rad | 99.01 deg |
Sweep (1/4 c) | 0.4422 rad | 25.34 deg |
Volume Coefficient | 0.01959 | |
Control Surface | Rudder | |
% Span | 99.8 | |
Mean % Chord | 48.39 | |
Inboard Edge (% semi span) | 0.149 | |
Control Area | 0.5842 m^2 | 0.5842 m^2 |
Affected Wing Area | 1.207 m^2 | 1.207 m^2 |
Parameter | SI Units | User Units |
---|---|---|
Ref Position X | 2.19 m | 2.19 m |
Y | 0.0 m | 0.0 m |
Z | -0.3533 m | -0.3533 m |
Aerodynamic Center Position | 3.173 m | 3.173 m |
Ref Area | 4.714 m^2 | 4.714 m^2 |
Exposed Area | 2.262 m^2 | 2.262 m^2 |
Wetted Area | 9.62 m^2 | 9.62 m^2 |
Span | 1.966 m | 1.966 m |
Fuselage Cutout | 0.4135 m | 0.4135 m |
Mean Aerodynamic Chord | 2.04 m | 2.04 m |
Aspect Ratio | 0.8204 | |
Root Airfoil Section | 2412 | |
Root Airfoil Thickness | 12 | |
Tip Airfoil Section | 2412 | |
Tip Airfoil Thickness | 12 | |
Root Chord | 3.371 m | 3.371 m |
Tip Chord | 1.423 m | 1.423 m |
Taper Ratio | 0.4222 | |
Root Incidence | 0.05236 rad | 3. deg |
Twist | 0.0 rad | 0.0 deg |
Dihedral | -0.05389 rad | -3.088 deg |
Sweep (1/4 c) | 0.9756 rad | 55.9 deg |
Parameter | SI Units | User Units |
---|---|---|
Ref Position X | -8.721e-04 m | -8.721e-04 m |
Y | 0.0 m | 0.0 m |
Z | -0.3823 m | -0.3823 m |
Max Width | 1.006 m | 1.006 m |
Max Height | 1.287 m | 1.287 m |
Length Overall | 4.894 m | 4.894 m |
Frontal Area | 1.017 m^2 | 1.017 m^2 |
Wetted Area | 12.31 m^2 | 12.31 m^2 |
Volume | 2.89 m^3 | 2.89 m^3 |
Parameter | SI Units | User Units |
---|---|---|
Ref Position X | 1.983 m | 1.983 m |
Y | 0.0 m | 0.0 m |
Z | 0.093 m | 0.093 m |
Number of Passengers | 1 | |
Seats Across | 0 | |
Rows | 0 | |
Seat Pitch | 1.27 m | 1.27 m |
Width | 0.0 m | 0.0 m |
Height | 1.232 m | 1.232 m |
Length | 1.27 m | 1.27 m |
Parameter | SI Units | User Units |
---|---|---|
Gear Configuration | Tricycle | |
Main Position X | 4.564 m | 4.564 m |
Y | 0.0 m | 0.0 m |
Z | -1.271 m | -1.271 m |
Main Diameter | 0.432 m | 0.432 m |
Main Width | 0.1582 m | 0.1582 m |
Nose Position X | 0.7217 m | 0.7217 m |
Y | 0.0 m | 0.0 m |
Z | -1.343 m | -1.343 m |
Nose Diameter | 0.3024 m | 0.3024 m |
Nose Width | 0.1108 m | 0.1108 m |
Wheel Base | 3.843 m | 3.843 m |
Main Track | 2.03 m | 2.03 m |
Parameter | SI Units | User Units |
---|---|---|
Tank Type | Wing Tank | |
Ref Position X | 3.289 m | 3.289 m |
Y | 0.0 m | 0.0 m |
Z | -0.4567 m | -0.4567 m |
Fuel Volume | 0.177 m^3 | 177. liter |
Fuel Weight | 124.3 kg | 124.3 kg |
% Span | 20.05 | |
Inboard Edge (% Semispan) | 1.217 | |
% Chord | 47.55 | |
Forward Edge (% Chord) | 2.803 |
Parameter | SI Units | User Units |
---|---|---|
Ref Position X | 1.38 m | 1.38 m |
Y | 0.01294 m | 0.01294 m |
Z | -0.1281 m | -0.1281 m |
CG Position | 1.38 m | 1.38 m |
Weight | 22.68 kg | 22.68 kg |
Width | 0.305 m | 0.305 m |
Height | 0.305 m | 0.305 m |
Length | 0.305 m | 0.305 m |