COMPBL-II - Compressible, Variable Pressure Boundary Layer Program for Arbitrary Gaseous Mixtures

Abstract

A code has been written to calculate the boundary layer over a body for a compressible, variable pressure flow with an arbitrary gaseous mixture. This code was written to handle internal flows as well as external flows. For this reason, combustion gases at elevated temperatures are of interest and are treated. The boundary layer equations are solved using an integral technique.

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Document Details

Document Type
Technical Report
Publication Date
Oct 01, 1981
Accession Number
ADA131352

Entities

People

  • B. J. Walker
  • T. A. Antoon

Organizations

  • United States Army Aviation and Missile Command

Tags

Communities of Interest

  • Air Platforms
  • Cyber
  • Weapons Technologies

DTIC Thesaurus Topics

  • Air Force
  • Boundary Layer
  • Boundary Layer Flow
  • Equations
  • Flow
  • Geometry
  • Heat Transfer
  • Layers
  • Mach Number
  • Plane Geometry
  • Plastic Explosives
  • Reynolds Number
  • Specific Heat
  • Thermal Conductivity
  • Transport Properties
  • Two Dimensional
  • Variable Pressure

Fields of Study

  • Physics

Readers

  • Combustion science or combustion engineering.
  • Computational Linguistics
  • Fluid Dynamics.