Accession Number : ADA299898

Title :   Preliminary Study on Effects of Thrust Vectoring,

Corporate Author : NATIONAL AIR INTELLIGENCE CENTER WRIGHT-PATTERSON AFB OH

Personal Author(s) : Baokai, Zhao

PDF Url : ADA299898

Report Date : 01 AUG 1995

Pagination or Media Count : 17

Abstract : With respect to the thrust vectoring technique adopted in aircraft, the paper is a preliminary study on the pneumatic properties, aircraft performance, and maneuverability after applying a two dimensional nozzle. Some conclusions are obtained.

Descriptors :   *FLIGHT MANEUVERS, *THRUST VECTOR CONTROL SYSTEMS, MANEUVERABILITY, PERFORMANCE(ENGINEERING), TWO DIMENSIONAL, NOZZLES, TRANSLATIONS, CHINA, CHINESE LANGUAGE, PNEUMATIC EQUIPMENT.

Subject Categories : Military Aircraft Operations

Distribution Statement : APPROVED FOR PUBLIC RELEASE