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Time (s)<br />
Mach Number<br />
<strong>Mig</strong>-<strong>21</strong>-FM-Identification-Rev. 14<br />
1.300<br />
1.200<br />
62<br />
1.15<br />
1.100<br />
41.5<br />
1.05<br />
1.000<br />
32.5<br />
0.95<br />
25.5<br />
0.900<br />
0.85<br />
19.5<br />
0.800<br />
0.75<br />
14<br />
0.700<br />
0.65<br />
8<br />
0.600<br />
0.55<br />
1.5<br />
0.500<br />
0.45<br />
0.400<br />
0.300<br />
0.00 10.00 20.00 30.00 40.00 50.00 60.00 70.00 80.00 90.00 100.00<br />
Time (s)<br />
Extracted<br />
Sampled<br />
Mach<br />
V(TAS) dV/dt Ps Ps Thrust<br />
m/s (m/s**2) (m/s) (ft/s) (lbs)<br />
0.50 168 5.18 89 291 11,374<br />
0.60 202 5.61 115 379 13,260<br />
0.70 235 6.12 147 482 14,826<br />
0.80 269 5.61 154 505 15,544<br />
0.90 303 4.81 148 487 16,311<br />
1.00 336 3.74 128 4<strong>21</strong> 19,915<br />
1.10 370 1.64 62 203 20,529<br />
The comparison between the computed data and the one extracted from the L-17 manual is<br />
summarized by the following figure: the computed values are displayed as B&W curves, the values<br />
extracted from manual are displayed as big dots.<br />
180<br />
165<br />
150<br />
135<br />
3,281<br />
9,843<br />
RL 1,000m<br />
Level <strong>Flight</strong> Acceleration<br />
120<br />
RL 3,000m<br />
105<br />
90<br />
75<br />
60<br />
45<br />
30<br />
15<br />
0<br />
0.30 0.40 0.50 0.60 0.70 0.80 0.90 1.00 1.10 1.20 1.30 1.40 1.50 1.60<br />
Mach<br />
Fig.15<br />
Page - 26
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