National Research Council of Canada. National Aeronautical Establishment. Structures and Materials Section.

• Elastic Suspension of A Rigid Body
• Fatigue Tests on Notched Specimens of 2024-T351 Aluminum Alloy Under A Low Altitude Aircraft Load Spectrum
• Finite Cylindrical Shell Element and the Vibrations of A Curved Fan Blade
• Finite Plate-Bending Elements in Polar co-Ordinates
• High Precision Triangular Plate-Bending Element
• Investigation of the Near Noise Fields of A Choked Axisymmetric Air Jet
• On Applying Finite Elements to Panel Flutter
• Profiles and Power Spectra of Some Off-Runway Landing Areas
• Stress Intensity Factors For A Crack Progressing Along A Series of Equally Spaced Holes
• Verification of the Nrc 3,000-Pound Standard Deadweight Machine
• Vibration Modes and Random Response of A Multi-Bay Panel System Using Finite Elements
• Vibration of Stepped Cantilevered Plates