Accession Number : ADA951880

Title :   Stability of Tapered Rectangular Plates under Varying Compression and Shear Loads.

Corporate Author : NORTH AMERICAN AVIATION INC DOWNEY CALIF

Report Date : 15 MAY 1958

Pagination or Media Count : 39

Descriptors :   *Plates, *Rectangular bodies, *Buckling, *Compression, *Shear stresses, *Taper, Metal plates, Processing, Milling machines, Stability, Test methods, Experimental data, Mathematical models, Computerized simulation

Subject Categories : Numerical Mathematics
      Test Facilities, Equipment and Methods
      Mechanics

Distribution Statement : APPROVED FOR PUBLIC RELEASE