Structural Integrity Investigation of Reworked S-2 Corrugated Wing Skin Panels.
NAVAL AIR DEVELOPMENT CENTER WARMINSTER PA AERO STRUCTURES DEPT
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Laboratory fatigue tests were performed on reworked S-2 corrugated wing skin panels to determine the effect on the structural integrity of skin material removal due to corrosion damage. Reworking of the S-2 aircraft corrugated wing skin panels, as performed by the Naval Air Rework Facilities, to remove corrosion damaged material, does not adversely affect the structural integrity of the panels. Author
- Patrol and Reconnaissance Aircraft