Accession Number:

ADA801471

Title:

The Limit of Stability of a Curved Plate Under Shear and Axial Stresses

Personal Author(s):

Corporate Author:

NATIONAL ADVISORY COMMITTEE FOR AERONAUTICS LANGLEY FIELD VA LANGLEY AERONAUTICAL LABORATORY

Report Date:

1939-06-01

Abstract:

For an infinitely long plate of constant curvature, the buckling condition for combined shear and axial stresses was set up. The buckling condition was evaluated for the case of pure shear and an approximate formula was derived for the critical stresses for large curvatures. In connection with the discussion of the methods and results, the range of validity of the bucking condition set up is defined.

Descriptive Note:

Technical memo.

Supplementary Note:

Translated from Die Stabilitaetsgrenze eines gekruemmten Plattenstreifens bei Beanspruchung durch Schub- und Laengskraefte, published by Luftfahrtforschung, Berlin-Adlershof (Germany East and West), v15 n10/11, 10 Oct 1938. Text in English.

Pages:

0036

Communities Of Interest:

Distribution Statement:

Approved for public release; distribution is unlimited.

File Size:

6.33MB