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pHelicopter (phys (rot(1:nRotor) # (R0, R, A, d_GH, V_R_H, tw, tw0, w,…
pHelicopter
phys
FL
S
k_dl
L
W
H
DT
nEng
P_avail
P_aux
eta
TR
R
c_d_mean
d_GH
rot(1:nRotor)
#
R0
R
A
d_GH
V_R_H
tw
tw0
w
nBlade
segmentCount
segments(1:segmentCount)
#
chord(1:segmentCount)
#
c_d_mean
profileData
v
mass
MTOW
nRotor
cfg
DRM
num
thetaDeviation
maxTrimIterations
richardsenOrder
DEFAULT_RRES
DEFAULT_PSIRES
nonLiftingPercent
errThr_ln
errThr_trim
errThr_dTheta
maxLineIterations
penaltyBorder
stepsR
stepsPsi
flags
enablePreconditioning
enableRandomPertubation
useRichardsonExtrapolation
trimActive
enableLineSearch
trimFromZero
enableBadCells
PCM
num
radialRes
circRes
flag
printOutput
model
MR
TR
PD
CLMB
AP
DT
BWK
flag
printAnnotation
useEngineModel
calcBeyondMax
savePlot
savePNG
saveFIG
savePDF
printSubPowers
printLegend
num
maxFTDCount
DEFAULT_VRES
DEFAULT_VMIN
campaingName
type
name
lastCall
res
DRM
rot(1:nRotor)
# :
F_H_HF
F_H_B
M_H_Hf
M_H_B
F_R0_H
F_R0Hf
M_R0_H
M_R0_Hf
M_G_B
F_G_A_B
M_G_A_B
E
J
H
err_ln
inflow
trimSuccessfull
badCellCount
PCM
P_MR
P_ind
P_TR
P_PD
P_C
P_ges
P_AP
P_DT
BWK
FTD
intermed
DRM
rot(1:nRotor)
#
theta
PCM
BWK