Accession Number:

ADA014367

Title:

Research and Development of Aircraft Control Actuation Systems. The Development of a Flight Control System Simulator, Research on a Control Surface Flutter Suppression Technique and High Temperature Testing of Mil-H-83282.

Descriptive Note:

Final rept. Jan 74-Feb 75,

Corporate Author:

DYNAMIC CONTROLS INC DAYTON OHIO

Personal Author(s):

Report Date:

1975-01-01

Pagination or Media Count:

202.0

Abstract:

This report presents the results of the following three research and development activities the design, fabrication and test of a multi-channel flight control system hybrid simulator the analysis and application of a flutter damping technique for hydraulically actuated slab type control surfaces and the experimental testing of Mil-H-83282 hydraulic fluid in a pumping system at elevated temperature.

Subject Categories:

  • Aircraft

Distribution Statement:

APPROVED FOR PUBLIC RELEASE