ow
6

2.

6

«ee

ee

ee

oe

wee

wee

Tv.
ate

re

versus Tine after Shock Arrival, Right
Horizontal Stabilizer Station 144, B-36D,

Shot

9...

ee

cece

cere

es

we

wc

eves

5.13

Shot 9.4. 6 2 ee we ee we ewe mre ewer ee
Vertical Acceleration versus Time after Shock
Arrival, B=36D Center of Gravity, Fuselage

Sy
ee

«cee

Vertical Acceleration versus Time after Shock

4

sot

«

5.12

“

RPSor.
eT

vv eve ery

9...

Vertical Acceleration versus Time after Shock
Arrival, B-36D Tail, Fuselage Station 1770,

5,14

By

Shot

5,11

eo

es

eo

ee

ww

we

eee

Arrival, B-36D Nose, Fuselage Station 212,

Station 907, Shot 9

2... 2. eee se ee oe

Stabilizer Shear (Point Loai Measurement)

.

~~

5.16

85
86

versus Time after Shock arrival, Left

Horizontal Stabilizer Station 62, Be36D,
5.15

83

Shot 9... 6

1

ee we ew we we ee ww eww os

Stabilizer Shear (Point Load Measurement)

87

versus Time after Shock arrival, Right

Horizontal Stabilizer Station 62, b=36D,
Shot 9... 6. 2 6 ew we et we we wee we ewe
Stabilizer Shear (Point Load Measurement)
versus -Time after Shock arrival, Right

Horizontal Stabilizer Station 144, %-36D,

Shot

“eee

CHAPTER 6

«©

2

«©

ee

ew

eo

eevee

es

ees

DISCUSSION
6.1

vor rene

9...

6.2
6.3

6.4

Peak Positive *ing Sending Moments Measure in
Mike, King, and Shot 9 Plotted versus ting

Station (Expressed as Distance in Inches from
Aircraft Center Line) . 2... 0. ee eee
Comparison cf sending Mecsurements made at
Station 62 of the Left Horizontal Stabilizer,

Be26D during Mike and Shot 9 .......-. 6
Comparison of Fuselage Eending Measurements

92
94

made at Station 1040 on the o~36D during Mike,
King and Shot 9. ww ww ew ee ew et ee ww
Comparison of Center of Gravity Acceleration

versus Time with Wing Bending (Station 110)
versus Time, >-36D, Mike Shot

. 2.1... 64.

98

TASLES
CHAPTER 2

PROOZEDURE
2.1

.

‘

poet

re wre ye pe

.

gt

2.2
2.3

33

Instrurentation, 5+36D nzircraft, IVY .

Instrurentation, 5-360 Em-renna-e
UPSHOT~ANOTHLLE

2

1.

ee

ew

eee

Instruvertetion, B-u73 aircraft, IVY .

Bar

.

.

37
40

-

we ae
ee eae
oie,
ees
eee
ae es
7

ee

-e

9.

tet tite
wtp
ies
(ae ara e WP ts

mon

armen
8 Ee

Shot

5.10 Stabilizer Bending (Point Load Measurement)

Select target paragraph3