operative prior to take-off and no recording was zttempted. 4.3.1.2 Acceleration Normal acceleration data for the tail, nose, and center of gravity are presented in Figs. 4.8 through 4.11. No usable data were obtained from the accelerometer in the left wing tip. The sharp spikes, characteristic of acceleration measurements of this type, have not been faired out. 4e3.123 Shear and Torsion Beth the shear gage and the torsion gage in the left outer wing panel were inoperative prior to the test; hence, no data for these response functions were obtained. bye3e2 Beh? Aircraft wae 7 ee ppm, SATE Siemans mere ee areatm OemSTNRT Cyt visit PERU ina ee pi ao... The 5-47 aircraft was essentially at intended position at blast arrival, The four response channels all produced usable data. The wing pending motent measurements are presented in Figs. 4.12 and 4.13; the vertical acceleration measurements are presented in Figs. 4.14 and 4.15. enal e “@ ® @ @ 6 6 o 88 eS a 2