Simulation of the Induced Flow through a Rotor in Descending Flight.

Abstract

The report outlines an emperical modification to classified momentum theory for the modeling of the induced flow through a rotor in descending flight. Consideration is also given to the computational stability of the procedure with emphasis upon the real-time representation of the system within a digital computer. (Author)

Document Details

Document Type
Technical Report
Publication Date
Jun 01, 1972
Accession Number
AD0745103

Entities

People

  • N. K. Shupe

Organizations

  • United States Army Communications-Electronics Command

Tags

DTIC Thesaurus Topics

  • Computers
  • Control Simulators
  • Digital Computers
  • Momentum
  • Simulations
  • Simulators

Fields of Study

  • Physics

Readers

  • Aerospace Engineering
  • Computational Fluid Dynamics (CFD)
  • Computer Science.