Accession Number : AD0644145

Title :   CONTROL OF SUPERSONIC AIRCRAFT,

Corporate Author : FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OHIO

Personal Author(s) : Sklyanskii,F. I.

Report Date : 31 MAY 1966

Pagination or Media Count : 385

Abstract : Contents: General information, equations of motion, definitions; Stability and controllability characteristics of aircraft, formation of forces on control levers of aircraft with non-power-assisted (boosterless) control systems; Change of characteristics of stability and controllability of aircraft at transonic and supersonic speeds of flight; Improvement of stability and controllability characteristics by methods of aerodynamic design and selection of shapes of supersonic aircraft; Power control formation of forces on aircraft control levers with power control; Application of automatic devices for improvement of characteristics of dynamic stability and controllability of present-day aircraft; Certain questions of the further development of control systems; The influence of deformation of the aircraft structure on its stability and controllability; Increase of safety of flight and emergency control.

Descriptors :   (*SUPERSONIC AIRCRAFT, CONTROL SYSTEMS), STABILIZATION SYSTEMS, MANEUVERABILITY, ROLL, CONTROL SURFACES, AERODYNAMIC CONFIGURATIONS, DEFORMATION, AVIATION SAFETY, USSR

Subject Categories : Aircraft

Distribution Statement : APPROVED FOR PUBLIC RELEASE