eCalc - performanceCalc

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Language:

Environment

Unit:
 
Elevation:
m ASL
Temperature:
°C
Take-off:
 

Drive Data

# Motors:
 
Ø Propeller:
inch
Propeller Pitch:
inch
# Blades:
Pcont/Tconst: (hide)
max. Revolutions:
rpm
max. Static Thrust:
g
Climb up to:
m AAL

Aircraft Data

All-up Weight:
g
Fuselage
Length:
mm
max. Effective Diameter:
mm
Wing
Area:
dm²
Span:
mm
Thickness:
%
Stabilizer
Area:
dm²
Span:
mm
Thickness:
%
Gear Area:
dm²
 
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Remarks:

Level Flight Performance


Speed Range

Rate of Climb

Time to Height

3D Capability
 
Power Diagram in Level Flight
Performance in the dynamic speed range and under static conditions (3D)
Air Speed [km/h]
 
Dynamic Climb Performance
Air Speed [km/h]
 

Vertical Performance


Acceleration

Vertical Speed
 
Static Vertical Climb
3D pull up performance
Time [s]
 

Airplane Performance

Aircraft Class:
-
 
Thrust-Weight-Ratio:
-
:1
Take-off Distance:
-
m
Stall Speed (clean):
-
km/h
Best Range (Carson) Speed:
-
km/h
max. Speed (Level):
-
km/h
Pitch Speed:
-
km/h
Zero Thrust Speed:
-
km/h
max. Propeller Power:
-
W
req. electric Power:
-
W
max. vertical Speed:
-
m/s
max. Angle of Climb:
-
°
max. Rate of Climb:
-
m/s
Time to Height:
-
s
Cd (normalized for wing area):
-

Version: P