Serial/Series Title

Dependence of the Elastic Strain Coefficient of Copper on the Pre-Treatment (open access)

Dependence of the Elastic Strain Coefficient of Copper on the Pre-Treatment

The effect of various pre-treatments on the elastic strain coefficient (alpha) (defined as the reciprocal of the modulus of elasticity E) (Epsilon) and on the mechanical hysteresis of copper has been investigated. Variables comprising the pre-treatments were pre-straining by stretching in a tensile testing machine and by drawing through a die, aging at room and elevated temperatures and annealing. The variation of the elastic strain coefficient with test stress was also investigated.
Date: August 1950
Creator: Kuntze, Wilhelm
System: The UNT Digital Library
Contribution to the Problem of Buckling of Orthotropic Plates, With Special Reference to Plywood (open access)

Contribution to the Problem of Buckling of Orthotropic Plates, With Special Reference to Plywood

Planar stress-strain relations and bending stress-strain relations are presented for elastic orthotropic plates and specialized to plywood. These relations are used to derive the differential equation and energy expression for the buckling of orthotropic rectangular plates whose principal stiffness directions are not parallel to the plate edges. Buckling analyses are made for the case of pure compression and pure shear of a long plate-strip.
Date: August 1950
Creator: Thielemann, Wilhelm
System: The UNT Digital Library
Investigations of Lateral Stability of a Glide Bomb Using Automatic Control Having No Time Lag (open access)

Investigations of Lateral Stability of a Glide Bomb Using Automatic Control Having No Time Lag

The investigation of the lateral stability of an automatically controlled glide bomb led also to the attempt of clarifying the influence of a phugoid oscillation or of any general longitudinal oscillation on the lateral stability of a glide bomb. Under the assumption that its period of oscillation considerably exceeds the rolling and yawing oscillation and that c(sub a) is, at least in sections, practically constant, the result of this test is quite simple. It becomes clear that the influence of the phugoid oscillation may be replaced by suitable variation of the rolling-yawing moment on a rectilinear flight path instead of the phugoid oscillation.
Date: August 1950
Creator: Sponder, E. W.
System: The UNT Digital Library