ANALYSIS OF LUG AND SWAY BRACE REACTIONS FOR THE XM19 AIRCRAFT POD.
SPRINGFIELD ARMORY MASS
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The maximum theoretical loads at the attachment points of the XM19 aircraft pod were determined. The load analysis as established by Military Specification MIL-A8591C was modified to include gun firing loads. The magnitude of the individual loads, the derivations of the pod reaction equations, and the sway brace reactions are included. Author