Thrust Vectoring Nozzle for Modern Military Aircraft

Abstract

This paper describes the technical features of the Thrust Vectoring Nozzle (TVN) developed by ITP and its advantages for modem military aircraft. It is presented in Conjunction with two other papers by DASA (Thrust Vectoring for Advanced Fighter Aircraft High Angle of Attack Intake Investigations) and MTU-Muenchen (Integrated Thrust Vector Jet Engine Control) respectively.

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Document Details

Document Type
Technical Report
Publication Date
May 11, 2000
Accession Number
ADP011109

Entities

People

  • Daniel Ikaza

Tags

Communities of Interest

  • Air Platforms
  • Space

DTIC Thesaurus Topics

  • Actuators
  • Aerodynamic Control Surfaces
  • Aircrafts
  • Computational Fluid Dynamics
  • Control Surfaces
  • Control Systems
  • Engines
  • Fighter Aircraft
  • Flight Control Systems
  • Fluid Dynamics
  • Gas Flow
  • Gas Turbine Nozzles
  • Geometry
  • High Pressure
  • Hydraulic Actuators
  • Military Aircraft
  • Three Dimensional

Fields of Study

  • Physics

Readers

  • Aerodynamics.
  • Naval Engineering and Maritime Security