Adjustment DA Max Gross Wt (HOGE)
NONE 7800 FT 34,800 lbs
10% RULE 8800 FT 34,000 lbs
DA COMPUTER 8400 FT 34,500 lbs
40% RULE 8400 FT 34,500 lbs
FF SCVqSCAF Vq
LL SCVqSCL Vq
DD SCVqSCD Vq
lSCVL V
bcRAS bA b c R
Rbc
RbcR
AAb
RRbbA
bA A
RAT
AA
RATc
bb
T
AbA
Therefore, the student is expected to become familiar with all NATOPS performance charts prior to class.
VA2T=Power
fDiskinduced
A
A2ThrustxThrust=Power
diskinduced
A
A2Thrust=v
diski A
A2ThrustxThrust=Power
diskinduced
A
everybody else skip this part
cdrRCP D
R
Oofile R
R
O
drRcCPR
ODofile
R
O
c
RcCP Dofile c
b=
PTotal = P Induced + P Profile
ihffinduced VVVV V
diskih A
ThrustVdA
VA2T=V
fDiskinduced
A
fDiskinduced VA
TPowerDAD
Rx=
VelocityTipBladeAircraftofVelocity=ratio)(advance
xx(a
b=
b23
tipDdProfile )4.65+(1VAC81=Power
A2Thrust=v
diski A
(b) Low Inertia .
thrustrotortotalcomponentverticalAOB v
AOBcomponentverticalthrustrotortotal v
ngam
ngmmgma
gmWngmT
mT
mW
mT
mWa
TWmaF
Z
Z
Z
ZZ
tav Z ta
tad v ta
mkftlbMass
ftlbsStiffness