Accession Number:

ADA142753

Title:

Fuselage Torsion of a CT4 Aircraft.

Descriptive Note:

Technical memo.,

Corporate Author:

AERONAUTICAL RESEARCH LABS MELBOURNE (AUSTRALIA)

Personal Author(s):

Report Date:

1983-12-01

Pagination or Media Count:

25.0

Abstract:

The fuselage torsion mode of a CT4 aircraft has been examined using an impulsive testing technique. The mode shape and natural frequency are presented. Author

Subject Categories:

  • Aircraft
  • Test Facilities, Equipment and Methods
  • Mechanics

Distribution Statement:

APPROVED FOR PUBLIC RELEASE