Accession Number : ADA134322
Title : Helicopter Flying Qualities Characteristics-CH-46E. Volume 3.
Descriptive Note : Final rept.
Corporate Author : BOEING VERTOL CO PHILADELPHIA PA
PDF Url : ADA134322
Report Date : 03 Oct 1983
Pagination or Media Count : 206
Abstract : This volume contains transient time-history data extracted from the CH-46E SLEP II flight test program conducted at the Boeing Vertol flight test facility from 20 June to 31 October 1977. Four general types of data record are presented: Dynamic stability (longitudinal pulse response); Control responses (longitudinal, lateral and directional step response); SAS failure (longitudinal, lateral and directional hardover SAS input); and Engine failure (single engine step reduction to ground idle). In each record, the response of the helicopter in the axis of disturbance (control input, SAS failure, etc.) is thoroughly described by time-histories of six to eight relevant parameters in that axis, while interaxis coupling is assessed by a sampling of four parameters from each of the remaining axes.
Descriptors : *Helicopters, Flight maneuvers, Trim(Aerodynamics), Flight testing, Aerodynamic stability, Flight control systems, Response, Pulses, Augmentation, Failure, Helicopter rotors, Transients, Aircraft engines, Handling, Quality, Flight envelope, Experimental data, Parameters
Subject Categories : Flight Control and Instrumentation
Distribution Statement : APPROVED FOR PUBLIC RELEASE