Project 5.5 - In-Plight Participstion of an P-84P Aircraft - lt J.A, Sabatella Waiter (Capabilities P-84F) - This participation wes an atteapt to determine the capability of the P-84F aircraft by subjecting it to both thermal oni -eymmetric blast loeds. Barley (Sideloads F-84P) - The objective of this participation was to etudy the dynamic response of fighter structures to anti-symmetrio blast loads. TEEEREPTAL Waiter - 100 data channels vere available to record moment, shear, and torsion loads; accelerations, overpressure, temperature, thermal strain, and aireraft attitude. Out of these channels there vere four channels that failed. Barley - Out of the 100 channels available to record essentially the sem information as above, there were no channel failures. POSITION Waiter - At tige sero, the aircraft was flying at an altitude of 19,920 feet on an inbound hesding of 070.8, 52 feet offeet. The horisontal range was 3,729 feet and. The shock arrival position waa 2,129 feet altitude, 19,532 feet horisontal range and 2,566 feet offset to the right. Barley - At time sero, the aircraft wee flying at an altitude of 23,318 feet om an inbound heeding of 060.4%, ‘The herisontal range and offeet vere 16,653 feet and 22,237 feet respectively. At shook arrival, the aircraft vas at 23,075 feet altitude, 22,443 feet offeet, and 3,757 feet horisontel renge. BEST AVAILABLE = COPY -39- - pen’ »