Accession Number:

AD0644145

Title:

CONTROL OF SUPERSONIC AIRCRAFT,

Descriptive Note:

Corporate Author:

FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OHIO

Personal Author(s):

Report Date:

1966-05-31

Pagination or Media Count:

385.0

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.

Subject Categories:

  • Aircraft

Distribution Statement:

APPROVED FOR PUBLIC RELEASE