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Stress-Intensity Factor Solutions for Tapered Lugs with Oblique Pin Loads
Fractographic Examination of the Vertical Stabilizer and Rudder from American Airlines Flight 587
Induced Rolling Moment Characteristics of the M557A Bomb at Mach Number 0.50 Streamline
Some Applications of Aeronautical Engineering in the Construction of Yachts
Strength Behaviour of Fatigue Cracked Lugs (Festigkeitsverhalten von Rissbehafteten Augenstaeben)