Development of a Flight Simulation Concept and Aerodynamic Buildup for Investigation of Departure Prevention Systems in Tactical Aircraft.

Abstract

The conceptual development of a computer flight simulation for design, testing and analysis of departure prevention systems, simulation capability and programming are discussed, along with required research material and data. A description is given of the aerodynamic buildup program written for incorporation in the simulation, including the aerodynamic equations of the model base aircraft, sample program statements and output.

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Document Details

Document Type
Technical Report
Publication Date
Sep 01, 1983
Accession Number
ADA136182

Entities

People

  • A. L. Raithel Iii

Organizations

  • Naval Postgraduate School

Tags

Communities of Interest

  • Air Platforms
  • Space

DTIC Thesaurus Topics

  • Aeronautical Engineering
  • Aircraft Design
  • Aircrafts
  • Automatic Pilots
  • Computer Programming
  • Computers
  • Control Surfaces
  • Control Systems
  • Equations
  • Flight Control Systems
  • Horizontal Stabilizers
  • Leading Edge Flaps
  • Materials
  • Plastic Explosives
  • Research Facilities
  • Tactical Aircraft
  • United States Naval Academy

Fields of Study

  • Physics

Readers

  • Aviation Science / Aeronautics.
  • Computational Linguistics
  • Systems Analysis and Design