Development of Theoretical Models and Description of Computer Program. Volume I.

Abstract

Numerical computer models for the prediction of aircraft and missile exhaust plume flow fields are described. The flow model is capable of treating multiple shock waves in the exhaust plume. An infrared computer model is described and typical results are presented for some typical missile exhaust plumes. (Author)

Document Details

Document Type
Technical Report
Publication Date
Sep 15, 1976
Accession Number
ADA030380

Entities

People

  • Kenneth E. Harwell

Organizations

  • Auburn University

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Aircrafts
  • Computer Programs
  • Computers
  • Exhaust Plumes
  • Flow
  • Flow Fields
  • Plumes
  • Shock
  • Shock Waves
  • Waves

Readers

  • Aerospace Propulsion Engineering.
  • Computational Modeling and Simulation
  • Computer Science.