TABLE 6.2
DATA SUMMARY, B-36
Shot
Radient Exposure, cal/em't
1
2
4
5
6*
Max irradiance, cal/om'-seet
62
478
35.2
17.4
45.9
_
Max Temperature Rise of Elevater Skin
62
45
37
“
~
Max Overpreseure, pal
Max Pressure, pai, ew unteraide of:
0.81
0.56
0.42
0.60
0.22
Wing
0.90
0.62
0.48
0.68
0.27
Stabilizer
1.20
0.83
0.60
6.86
0.25
at Station 144.8, pareent of 400 F limit
Fuselage
0.92
0.64
0.48
—~
1.2
3.7
5.2
0.67
0.28
Max Positive Bending Moments, §
percent of Limit#:
Stabilizer, Station 62
59
60
37
18
27
Fuselage, Station 1476
Wing, Station 1062
50 to 70
5&0
47 to 87
50
22 ta 42
44
67 to 87
63
4 to 20
49
* Head-on orientation.
t Average of multiple instrumentation.
{ Temp-tape data.
§ Max positive bending moments are the peak incremental bending plus dead weight and in-flight
conditions.
TBending moment limits are defined as two thirds the static test ultimate.
TABLE 6.3
DATA SUMMARY, B-47
Shot 3 data unusable because of low yield. No participation in Shot 5.
Shot
1
2
4
6
Radiant Exposure, * cal/cm*
32.1
17.5
16.3
11.8
Max Irradiance, * cal/om*-sec
6.27
2.67
4.10
5.33
Time to Peak Irradiance, seconds
3.81
3.24
2.41
1.33
Duration of Irradiance, seconds
48
46
33
12
Peak Temperature Right Stabilizer, F
134
44
81
99
Time to Peak Right Stabilizer Temperature, seconds
9.0
10.0
7.0
5.0
Time to Shock Arrival (Station 1217), seconds
110.5
189.2
116.9
73.66
Peak Overpressure, psi
0.31
0.22
0.26
0.25
Peak c.g. Acceleration, g's
0.38
0.32
0.28
_
* Corrected to zero incident angle.
77