Charts are presented for the coefficients in the formulas for the critical compressive stress at which cross-sectional distortion begins in thin-wall columns of I-, Z-, channel, and rectangular-tube sections. The energy method of Timoshenko was used in the theoretical calculations required for the construction of the charts. The deflection equations were carefully selected to give good accuracy. The calculation of the critical compressive stress at stresses above the elastic range is briefly discussed in order to demonstrate the use of the formulas and the charts in engineering calculations. Two illustrative problems are included
The pack method for determining compressive stress-strain graphs described in NACA Report No. 649 ha...
When thin-walled columns formed from flanged sheet, such as used in airplane construction, are subje...
Direct-reading design charts are presented for 75S-T6 aluminum-alloy flat compression panels having ...
Charts are presented for the coefficients in formulas for the critical compressive stress at which c...
A chart is presented for the coefficient in the formula for the critical compressive stress at which...
Charts are presented for the coefficients in the formulas for the critical compressive stress at whi...
A chart is presented for the coefficient in the for-mula for the critical compressive stress at whic...
A chart is presented for the coefficient in the formula for the critical compressive stress at which...
Charts are presented for the coefficients in formulas for the critical compressive stress at which c...
A chart is presented for the values of the coefficient in the formula for the critical compressive s...
A chart is presented for the values of the coefficient in the formula for the critical compressive s...
A chart is presented for the values of the coefficient in the formula for the critical compressive s...
A method is presented for calculating crippling stresses of structural sections as a function of mat...
A solution is presented for the problem of the buckling of curved rectangular panels subjected to co...
Empirical design curves are presented for the critical stress of thin-walled cylinders loaded in axi...
The pack method for determining compressive stress-strain graphs described in NACA Report No. 649 ha...
When thin-walled columns formed from flanged sheet, such as used in airplane construction, are subje...
Direct-reading design charts are presented for 75S-T6 aluminum-alloy flat compression panels having ...
Charts are presented for the coefficients in formulas for the critical compressive stress at which c...
A chart is presented for the coefficient in the formula for the critical compressive stress at which...
Charts are presented for the coefficients in the formulas for the critical compressive stress at whi...
A chart is presented for the coefficient in the for-mula for the critical compressive stress at whic...
A chart is presented for the coefficient in the formula for the critical compressive stress at which...
Charts are presented for the coefficients in formulas for the critical compressive stress at which c...
A chart is presented for the values of the coefficient in the formula for the critical compressive s...
A chart is presented for the values of the coefficient in the formula for the critical compressive s...
A chart is presented for the values of the coefficient in the formula for the critical compressive s...
A method is presented for calculating crippling stresses of structural sections as a function of mat...
A solution is presented for the problem of the buckling of curved rectangular panels subjected to co...
Empirical design curves are presented for the critical stress of thin-walled cylinders loaded in axi...
The pack method for determining compressive stress-strain graphs described in NACA Report No. 649 ha...
When thin-walled columns formed from flanged sheet, such as used in airplane construction, are subje...
Direct-reading design charts are presented for 75S-T6 aluminum-alloy flat compression panels having ...