Accession Number:

AD0602563

Title:

SOME ACCURATE SOLUTIONS OF THE PROBLEM OF NATURAL VIBRATIONS OF A SWEPT-BACK WING IN A SUPERSONIC FLOW OF GAS,

Descriptive Note:

Corporate Author:

FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OHIO

Personal Author(s):

Report Date:

1963-12-27

Pagination or Media Count:

14.0

Abstract:

The investigation conducted on the problem of natural vibrations in a swept-back wing with constant chord with a coincidence of the flexural axis and the axis of the centers of mass of the wing permits the following qualitative conclusions. During purely torsional and combined flexural and torsional disturbed motions of the wing, flutter and divergence are impossible with identical frequency. During purely flexural motions it is possible for flutter and divergence to occur. Author

Subject Categories:

Distribution Statement:

APPROVED FOR PUBLIC RELEASE