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Questionaire Aircraft

Propeller

[mm] *

*


right hand
left hand


pusher
tractor


fixed pitch
constant speed
ground adjustable
adjustable in flight


feathering

Engine

at RPM

at RPM

/

Aircraft

D15 = [ ]

R/C = [ ]

VY = [ ]

VH = [ ]

VNO = [ ]

VNE = [ ]

Special design points:

Condition h
[ft/m]
Temp
[ºC/F]
P
[kW/hp]
rpm V
[kts/mph]
T
[N/lbs]
Static
Climb
Cruise

climb compromise cruise

yes no

Spinner

L = [mm/inch]

D = [mm/inch]

A = [ º ]

F = [mm/inch]

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