Stability and Controllability of Supersonic Aircraft,

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)

Document Details

Document Type
Technical Report
Publication Date
Dec 04, 1970
Accession Number
AD0719804

Entities

People

  • E. Galashev
  • V. Lutskii

Organizations

  • National Air and Space Intelligence Center

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Aircrafts
  • Airframes
  • Buffeting
  • Coefficients
  • Delta Wings
  • Flight Speeds
  • Jet Aircraft
  • Maneuverability
  • Overload
  • Supersonic Aircraft
  • Vehicles

Fields of Study

  • Physics

Readers

  • Aerodynamics/Aeronautics.
  • Mathematics or Statistics

Technology Areas

  • Hypersonics