Accession Number:

AD0705368

Title:

AEROELASTIC EFFECTS FROM A FLIGHT MECHANICS STANDPOINT.

Descriptive Note:

Conference proceedings.

Corporate Author:

ADVISORY GROUP FOR AEROSPACE RESEARCH AND DEVELOPMENT PARIS (FRANCE)

Personal Author(s):

Report Date:

1970-03-01

Pagination or Media Count:

415.0

Abstract:

The document is comprised of 27 papers grouped under the following headings The state-of-the-art Flight dynamics of a flexible VTOL rotor Flight dynamics of flexible airplanes theoretical methods Experimental methods for flight dynamics of the flexible airplane Stability and control augmentation devices.

Subject Categories:

  • Aerodynamics
  • Helicopters
  • Bombers
  • VSTOL

Distribution Statement:

APPROVED FOR PUBLIC RELEASE