Pete's  Planes

 

return to Homepage

 

return to Tech index

 
 
Flight Analysis No1

Commuter

Date of test flight 18 Sept 05

Data recorded with EagleTree V2 onboard datalogger.

 

Model Data.........motor--Jamara 480HS BB........prop--Master Electric 10"D 7"P [measured zero-thrust pitch is 8.3"] ............gear ratio 3.0.......span 62"........wing area 2.65 sq ft..............AR = 10.............weight 45 ozf = 12.5N............wing loading 17 oz/sq ft

 

   

initial climb

slow climb

level cruise

shallow glide

 timeline  secs  950--960  960--990  1050--1090  1090--1110
 battery out power  W  160 105 65 zero
power/weight W/lb 57 37 23 zero
airspeed mph 22 25 25 25
m/s 9.8 11.2 11.2 11.2
prop speed rpm 5700 4600 4000 --
pitch speed mph 45 36 31 --
rate of climb ft/sec 6.5 2.1 zero -3.4
ft/min 390 126 zero -204
m/s 2.0 .64 zero -1.04
 angle of climb or glide sine 1/4.9 1/17.5 zero 1/10.8
degrees 11.8 3.3 zero 5.3
tangent 1/4.8 1/17.5 zero 1/10.7
gravity power [A] W 25 8 zero -12.95
drag power [B] W 8.8 12.95 12.95 12.95
flight power [A+B] W 33.8 20.95 12.95 zero
overall propulsion efficiency   21% 20% 20% --
Highlighted values obtained from graph.

 

Revision  16 Oct 05 : Pitch speeds calculated using measured pitch [previously with nominal pitch].