Accession Number : AD0674211

Title :   FLIGHT TEST OF A HONEYWELL, INC., FLUIDIC YAW DAMPER

Descriptive Note : Final rept.

Corporate Author : BELL HELICOPTER TEXTRON INC FORT WORTH TX

Personal Author(s) : Kidwell, John C

PDF Url : AD0674211

Report Date : Jul 1968

Pagination or Media Count : 50

Abstract : Flight tests were conducted to evaluate the performance and feasibility of a fluidic yaw damper system. A standard UH-1C helicopter was used as a test vehicle.

Descriptors :   *FLUID AMPLIFIERS, *HELICOPTERS, CAPTIVE TESTS, DAMPING, FEASIBILITY STUDIES, FLIGHT CONTROL SYSTEMS, FLIGHT TESTING, HANDLING, HOVERING, LEVEL FLIGHT, PERFORMANCE(ENGINEERING), STABILITY, TEMPERATURE CONTROL, YAW

Subject Categories : Helicopters
      Fluidics and Fluerics

Distribution Statement : APPROVED FOR PUBLIC RELEASE