Accession Number:

ADA801312

Title:

A Method of Calculating Bending Stresses Due to Torsion

Personal Author(s):

Corporate Author:

NATIONAL AERONAUTICS AND SPACE ADMIN LANGLEY RESEARCH CENTER HAMPTON VA

Report Date:

1942-12-01

Abstract:

Analysis is given of bending stresses caused by torsion in a box with variable cross section and loading. Recurrence formula leads to set of equations identical in form with three-moment equations. Special formulas are provided for full-width cutouts and carry-through bays. Short-cut method in solving system of equations sufficiently accurate in practical stress analysis is indicated, which may be applied without knowledge of the general method.

Descriptive Note:

Wartime rept.

Pages:

0042

Identifiers:

Communities Of Interest:

Distribution Statement:

Approved for public release; distribution is unlimited.

File Size:

2.49MB