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Prediction of delamination in composite helicopter rotor and airframe structures

Wisnom, M.R.; Hill, G.F.J.; Jones, M.I. (2002)
Bearingless main rotor hub concept using precured carbon fibre rods in a flexible matrix

Potter, K.D.; Wisnom, M.R. (2002)
Post-buckling design and testing of composite stiffened cylindrical shells under torsion

Lanzi, L.; Bisagni, C.; Cordisco, P. (2003)
Industrial applications of shearography for inspection of aircraft components

Krupka, R.; Walz, T.; Ettemeyer, A. (2003)
Flaw tolerance substantiation test results for S-92 dynamic components

Adams, D.O.; Tritsch, D.E. (2002)
Identification of constitutive model parameters for crashworthiness of composite structures using multiobjective optimization

Anghileri, M.; Lanzi, L.; Mentuccia, F. (2003)
Brazier effect in spinning hollow composite drive shaft using mixed finite element method

Kumar, P.; Harursampath, D. (2004)
Attaining flaw-tolerant design life objectives in helicopter rotor system lugs

Mariani, U.; Ratti, G.; Reid, L. (2004)
A numerical model for hail impact analysis

Anghileri, M.; Castelletti, L.-M.L.; Invernizzi, F.; Mascheroni, M. (2004)
Preliminary study on structural properties of active twist blades

Riemenschneider, J.; Wierach, P.; Keye, S. (2003)

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