Aeroelastic Analysis of a Composite Wing Designed for the BQM-34E Supersonic Aerial Target Vehicle
Aerothermoelasticity of advanced composite swept aircraft wings: response and flutter instability
A method of calculating bending stresses due to torsion
An Extension of FASTSIM for Steady State Non-Hertzian Contact
An Improved Photoelastic Method for Determining Plane Stresses
A Normal Stress Amplifier for the Second Normal Stress Difference
Bending of rectangular plates with large deflections
Beryllium Fabrication Methods Development Program - Thermal Treatment
Bodies of Constant Stress Experiencing Forces of Orbital Flight
Buckling stresses of simply supported rectangular flat plates in shear
Comparison of Discrete Velocity Method and Gas-Kinetic Method for Binary Gas Mixtures
Compressive buckling of simply supported plates with transverse stiffeners