EASY-ACLS Dynamic Analysis. Volume I. Component Mathematical Models.

Abstract

Mathematical models were developed for a variety of Air Cushion Landing System components which include aircraft flight model components, wind, engine and air flow components, inelastic-elastic-trunk and cushion, air bag skid and arresting gear model components etc. The models were developed for utilization in the EASY-ACLS dynamic analysis computer program simulation. (AUTHOR)

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Document Details

Document Type
Technical Report
Publication Date
Sep 01, 1978
Accession Number
ADA080634

Entities

People

  • G. S. Duleba
  • J. R. Kilner
  • M. K. Wahi
  • P. R. Perkins

Organizations

  • Boeing Military Aircraft

Tags

Communities of Interest

  • Air Platforms
  • Energy and Power Technologies
  • Space

DTIC Thesaurus Topics

  • Aerodynamic Forces
  • Air Pressure
  • Air Supplies
  • Aircrafts
  • Boundary Layer
  • Computational Fluid Dynamics
  • Computational Science
  • Computer Programs
  • Computer Simulations
  • Control Systems
  • Coordinate Systems
  • Differential Equations
  • Dynamic Response
  • Equations Of Motion
  • Flow Rate
  • Geometry
  • Mathematical Models

Readers

  • Aerospace Engineering
  • Computational Modeling and Simulation
  • Logistics and Supply Chain Management.