STRUCTURAL TESTS OF FLIGHT DECK ON USS HANCOCK (CVA 19) UNDER SIMULATED A3D-1 AND F2H-3 AIRCRAFT LANDING LOADS,
Abstract
Static and dynamic strains and deflections were measured on the flight-deck structure of USS HANCOCK (CVA 19) after Project 27-C conversion. A specially designed loading apparatus was used for simulating wheel loadings of A3D-1 and F2H-3 aircraft. It is concluded that the present Bureau of Ships design method is accurate for calculating the stresses in the steel supporting structure for a wood-planked flight deck, and that failure of the planking will not occur at loads less than those determined by the design calculations. Also, the test results show that design based on initial yielding of the steel supporting structure is conservative. (Author)
Document Details
- Document Type
- Technical Report
- Publication Date
- Apr 01, 1959
- Accession Number
- AD0650301
Entities
People
- Ralph B. Allnutt