EasyManua.ls Logo

Douglas A-4M - Page 46

Douglas A-4M
68 pages
Print Icon
To Next Page IconTo Next Page
To Next Page IconTo Next Page
To Previous Page IconTo Previous Page
To Previous Page IconTo Previous Page
Loading...
Section
XI
Part
4
!
~
~
F::tf~:~
~::~
::
e::
e:~~~
of
Fu
el
(F)
Thr
us
t
required
/ f, umb -
I!
(G)
:1~::::i:l::::1:l1lher.
(
lI)
Dr
ag
index . . . . .
(J)
Total
thrust
requi
red
/
.5
arllb
!
!
I
!
S
AMPLE
NAUTICAL
MILES
PER
POUND OF FUEl
Naut
icol Miles
pe
t Pou
nd
of
Fuel
(For
fi
gu
re
11
- 30.
sheet
3)
IK)
Ambie
nt
ai
r
temp
er
ature
IL)
Pre
ss
ure
altitude
1M)
Cruise
Mach
number
.
IN)
Reynolds numb
er
index (
RNI
)
11-
58
NAVAlR
01-40AVM-l
6225
0.75
100
8820
FlI.l-\I>O
_44.40C
30.000
ft
0.75
0.503
SAMPLE NAUTICAL
MILES
PER
POUND OF FUEl
Nauticol Mil
es
pe
r P
ound
of
Fu
el
(For fib'Ure 11-30,
sheet
4)
IP)
To
tal
thrust
r
equired!
S
amb
IQ)
Cruise
M
ach
number
. .
IR)
Gene
ralized
fuel [low
paramet
er
(uncor
re
cte
d
for
Re
ynolds
numb
er
effe
ct)
IS)
Reynolds
number
index (RNI)
IT)
Generalized
fuel [low
pa
r
am
ete
r (co
rrected
for
Re
ynolds
numbe
r
effect
)
FlI.l-l61
8820 Ib
. 0. 75
6.2
3
0.503
6.41