A bomber easyto designthe aircraft around that center of gravity
Both axesoriginatefrom the centre of gravity of the aircraft
to be located along the center line of the fuselage and approximately near the center of the middle wing spar(passive) is designedThe aircraft center of gravity
Fuselage 206setsa low aircraft center of gravity
The low fuselage 101setsa low aircraft center of gravity
Fuselage 106setsa low aircraft center of gravity
the two sets of nozzlesbeing setabout the aircraft 's centre of gravity
to be within a certain range dependent on how the aircraft is loaded(passive) is very carefully designedThe center of gravity of an aircraft
Portland IQcreatescenter of gravity ” for
around the pilot in that locationwas designedaround the pilot in that location
in the Takeoff CG within limitsresultsin the Takeoff CG within limits
unintentional Tip - Back. Figure 4.16to preventunintentional Tip - Back. Figure 4.16
at 0 % static marginis setat 0 % static margin
at −5 % static marginis setat −5 % static margin
the aircraft ’s angle of attack problemcausedthe aircraft ’s angle of attack problem
from modifications or repaintingresultingfrom modifications or repainting
particularly when flying without any baggage in the nosecan resultparticularly when flying without any baggage in the nose
the aircraft to climb as a steep anglecausedthe aircraft to climb as a steep angle
to mount a pair of large radial ( piston ) engineswas ... designedto mount a pair of large radial ( piston ) engines