Accession Number:

ADA007450

Title:

Stability Analysis of the Torsional Bending Vibrations of Wing in a Subsonic Flow by Method of the Final Elements,

Descriptive Note:

Corporate Author:

FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OHIO

Personal Author(s):

Report Date:

1975-02-14

Pagination or Media Count:

33.0

Abstract:

Subject Categories:

  • Aerodynamics

Distribution Statement:

APPROVED FOR PUBLIC RELEASE