Accession Number:

ADA024480

Title:

The Design, Analysis and Testing of a Low Budget Wind Tunnel Flutter Model with Active Aerodynamic Controls. Volume II.

Descriptive Note:

Final rept. 1 Dec 70-30 Nov 75,

Corporate Author:

TEXAS UNIV AT AUSTIN DEPT OF AEROSPACE ENGINEERING AND ENGINEERING MECHANICS

Report Date:

1976-01-01

Pagination or Media Count:

33.0

Abstract:

This report describes a low budget flutter model incorporating active aerodynamic controls for flutter suppression studies, concentrating on the interfering lifting surface flutter phenomenon in the form of a swept wing-tail configuration. A flutter suppression mechanism was first demonstrated on a simple semi-rigid three degree of freedom flutter model of this configuration employing an active stabilator control. These preliminary studies were extended to the analysis of a larger degree of freedom AFFDL wing-tail flutter model. The analytical and experimental design of a flutter suppression system for the AFFDL model is presented along with the results of a preliminary passive flutter test. Author

Subject Categories:

  • Aircraft
  • Fluid Mechanics

Distribution Statement:

APPROVED FOR PUBLIC RELEASE