Accession Number : AD0736487

Title :   Reduction in Flutter Instability of an Elastic Beam with the Rigid Empennage in Supersonic Flow,

Corporate Author : FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OHIO

Personal Author(s) : Selezov,I. T. ; Kovbasa,G. T.

Report Date : 18 NOV 1971

Pagination or Media Count : 14

Abstract : The possibility of the expansion of the region of dynamic elastic stability of a finned beam streamlined by a supersonic gas flow is investigated. In order to do this a system of automatic control, which consists of the object of control, measuring elements and actuators, is used.

Descriptors :   (*TAILS(AIRCRAFT), FLUTTER), SUPERSONIC CHARACTERISTICS, STABILITY, ELASTIC PROPERTIES, AUTOMATIC, USSR

Subject Categories : Aerodynamics
      Aircraft
      Fluid Mechanics

Distribution Statement : APPROVED FOR PUBLIC RELEASE