0.016(2.3) 0.368 at Mach 1.
D
C
1.23 kg/m
a
V a
2 4 2
1 1
2 2
4 4
(1.23)(340.3) 7.12 10 N/m
(7.12 10 )(27.84)(0.0368) 7.3 10 N
D
q p V
D = q S C
4
(8273)(9.8) 8.11 10 NW
4 5
(7.3 8.11) 10 1.541 10 ND + W
5
131.6 k N 1.316 10 NT = =
T D W
D
T
T D W at all altitudes.
3
At 2000 m, 275.16 K and 1.0066 kg/m
T
(1.4)(287)(275.16) 332.5 m/sec.
100 0.3
332.5
a RT
V
Ma
1 1
q V
3 3 3
81.08 10 2.243 10 48.28 10 N
32
48.28 10 5.84 m/sec
8273
F
a = m
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