A Record of the Australian Mirage Wing Fatigue Test
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[1] J. Mann,et al. Fatigue Lives of Specimens Representing Critical Locations in Mirage III Spars under Australian and Swiss Test Spectra , 1985 .
[2] P. B. Hovell,et al. The interpretation of strain measurements for flight load determination , 1964 .
[3] Alan Baker,et al. APPLICATION OF BFRP CRACK PATCHING TO MIRAGE III AIRCRAFT , 1980 .
[4] J Y Mann,et al. Improving the Fatigue Life of the Mirage IIIO Wing Main Spar. , 1984 .
[5] J. Mann,et al. The Use of Interference-Fit Bolts or Bushes and Hole Cold Expansion for Increasing the Fatigue Life of Thick-Section Aluminium Alloy Bolted Joints , 1983 .
[6] J Y Mann,et al. A Comparison of Fatigue Lives under a Complex and a Much Simplified Flight-by-Flight Testing Sequence. , 1984 .