TABLE 6.4 -COMPARISON OF MAXIMUM THEORETICAL AND MEASURED INPUTS
AND RESPONSES, B-36
Shot
1
2
%
5
50.8
47.5
33.4
35.2
22.8
17.4
53.8
45.9
—
_
0.78
0.81
0.56
0.56
0.44
¢.42
0.61
0.60
0.26
0.22
Temperature Rise; percent of critical rise of
elevator skin, 0.020-inches mag.
Theoretical
Measured
98
§2*
16
45
58
37
119
64T
—_—
_—
Bending Moment, percent of critical moment of
stabilizer at Station 62
Theoretical
Measured
60
59
49
60
40
37
69
76
27
27
Ra iiant Exposure, cal/cm?
Theoretical
Measured
Overpressure, psi
Theoretical
Measured
6
* Temp-tape data.
t For Station 144.5. At Station 312 where the paint was missing, the percent of critical temperature
rise was 81.
TABLE 6.5 COMPARISON OF MEASURED DATA WITH EXTRAPOLATIONS
TO ZERO-TIME POSITIONS, B-47
Measured: data as measured on the aircraft.
Zero-time: values of measured
data extrapolated to zero-time position.
Shot
1
2
4
6
28.8
33.7
18.2
19.7
19.8
21.3
13.8
14.7
29.6
85.2
16.3
18.4
18.7
16.6
11.7
11.8
Average Energy
Radiometers:
Measured, cal/cm?*
Zero-time, cal/cm*
Measurement duration, seconds
25
Calorimeters:
Measured, cal/om*
Zero-time, cal/em?
Measurement duration, seconds
25
16
10
25
25
15
10
5.3
5.7
2.7
29
4.1
4.2
5.4
5.6
4.8
8.1
2.8
3.1
3.6
8.8
47
6.2
Measured
3.81
3.25
2.40
1.33
Zero-time
3.85
3.29
242
1.35
Calorimeters:
Measured
Zero-time
3.80
3.95
3.22
2.97
2.40
2.60
1.37
1.35
Peak Irradiance, cal/om’-sec
Radiometers:
Measured
Zero-time
Calorimeters:
Measured
Zero-time
Time to Second Maximum, seconds
Radiometersa:
18