Accession Number : AD0719804

Title :   Stability and Controllability of Supersonic Aircraft,

Corporate Author : FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OHIO

Personal Author(s) : Lutskii,V. ; Galashev,E.

Report Date : 04 DEC 1970

Pagination or Media Count : 13

Abstract : To a great extent, the maneuverability of a supersonic fighter is determined by the value of the maximal available overloads which vary in relation to the flight speed and height. In its turn, the maximal available overload is affected by the maximally permissible value of lift coefficient and the reserve C(subscript y)--ranging from the balancing value in straight flight to the maximally permissible value. Satisfactory parameters of stability and controllability are retained in the delta-wing fighters under conditions of aerodynamic buffeting. (Author)

Descriptors :   (*SUPERSONIC AIRCRAFT, MANEUVERABILITY), (*DELTA WINGS, LIFT), STABILITY, SWEPTBACK WINGS, AERODYNAMIC LOADING, PERFORMANCE(HUMAN), BUFFETING, USSR

Subject Categories : Aerodynamics
      Aircraft
      Fluid Mechanics

Distribution Statement : APPROVED FOR PUBLIC RELEASE