Author:
Jones R.,Bridgford N.,Wallace G.,Molent L.
Publisher
Springer Berlin Heidelberg
Reference5 articles.
1. Baker A.A. and Jones R., Bonded repair of aircraft structures, Martinus Nijhoff Publishers, The Netherlands, 1988.
2. Baker A.A., Callinan R.J., Davis M.J., Jones R. and Williams J.G., Aplication of BFRP crack patching to Mirage III aircraft, J. Theoretical and Applied Fracture Mechanics 2, 1–5, (1984).
3. Molent L., Callinan R.J. and Jones R., Design of an all boron epoxy doubler reinforcement for the F-111C wing pivot fitting: Structural design aspects, J. Composite Structures 11 (1989) pp57–83.
4. Heller M., Williams J.F., Hill T. and Jones R., Increasing the fatigue life of cracked fastener holes using bonded repairs, J. Theoretical and Applied Fracture Mechanics 11, 1 (1989)
5. R. M. Bader, A review of research on aeronautical fatigue in the United States 1987–1989, ICAF National Reviews, Compiled by A. Berkovits, ICAF Document No 1681, 1989.
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8 articles.
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