A SIMPLE GRAPHICAL METHOD FOR EVALUATING THE EFFECT OF THRUST VECTOR TILT ON THE AIRCRAFT PERFORMANCE.

Abstract

The semi-graphical method presented in the report may be useful for the preliminary performance computation for an aircraft with the variable thrust axis tilt. Application to different flight problems is shown. Optimization of some flight parameters can be achieved by simple graphical construction. (Author)

Document Details

Document Type
Technical Report
Publication Date
Jul 01, 1968
Accession Number
AD0838391

Entities

People

  • Peter Bielkowicz

Organizations

  • Air Force Institute of Technology

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Aircrafts
  • Computations
  • Construction
  • Mathematical Analysis
  • Optimization

Readers

  • Aviation Science / Aeronautics.
  • Computational Modeling and Simulation
  • Materials Science and Engineering.