AirplanePDQ

Geometry Report

Design Name: P-5
Designer: Makarov A.V.
Design Date: 05.02.2007
File Name: C:\Program Files\AirplanePDQ\P-5_2.dwg

Engine #1

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

Propeller #1

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

Main Wing

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

Canard

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

Vertical Stabilizer

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

naplyv

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

Fuselage

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

Cabin

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

Landing Gear

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

Fuel Tank #1

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

Cargo (Cargo)

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
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