Accession Number : AD0720740

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 : 9

Abstract : A general description is given of methods by which a pilot can control the lateral motion of a supersonic aircraft.

Descriptors :   (*SUPERSONIC AIRCRAFT, STABILITY), (*FLIGHT CONTROL SYSTEMS, SUPERSONIC AIRCRAFT), ROLL, CONTROL STICKS, AERIAL RUDDERS, USSR

Subject Categories : Aircraft

Distribution Statement : APPROVED FOR PUBLIC RELEASE