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Flight Parameters Monitoring System for Tracking Structural Integrity of Rotary-Wing Aircraft
Mohammadi, J.; Olkiewicz, C. National Aeronautics and Space Administration 1994 p.505-516
Fatigue Loads Spectra Derivation for the Space Shuttle - Second Cycle
Ortasse, R. National Aeronautics and Space Administration 1994 p.517-546
Prediction of Fatigue Crack Growth under Flight-Simulation Loading with the Modified Corpus Model
Padmadinata, U. H.; Schijve, J. National Aeronautics and Space Administration 1994 p.547-562
The Characterization of Widespread Fatigue Damage in Fuselage Structure
Piascik, R. S.; Willard, S. A.; Miller, M. National Aeronautics and Space Administration 1994 p.563-580
Discrete Crack Growth Analysis Methodology for Through Cracks in Pressurized Fuselage Structures
Potyondy, D. O.; Wawrzynek, P. A.; Ingraffea, A. R. National Aeronautics and Space Administration 1994 p.581-602
A New Stochastic Systems Approach to Structural Integrity
Provan, J. W.; Farhangdoost, K. National Aeronautics and Space Administration 1994 p.603-620
Fatigue and Damage Tolerance Scatter Models
Raikher, V. L. National Aeronautics and Space Administration 1994 p.621-634
A Probabilistic Fatigue Analysis of Multiple Site Damage
Rohrbaugh, S. M.; Ruff, D.; Hillberry, B. M.; McCabe, G. National Aeronautics and Space Administration 1994 p.635-652
Evaluation of the Fuselage Lap Joint Fatigue and Terminating Action Repair
Samavedam, G.; Thomson, D.; Jeong, D. Y. National Aeronautics and Space Administration 1994 p.653-664
Fatigue Life until Small Cracks in Aircraft Structures. Durability and Damage Tolerance
Schijve, J. National Aeronautics and Space Administration 1994 p.665-682