Aerodynamic Heating Computations for Projectiles - Vol. 2: Swept Wing Calculations Using the Planar Version of the ABRES Shape Change Code (PLNRASCC).

Abstract

This report documents modifications and additions incorporated into the ABRES Shape Change Code (ASCC8O) to create a planar two-dimensional version of the axisymmetric computer code. This planar code predicts convective heat transfer and in-depth conduction for swept wings in supersonic flow. The report contains test cases and a detailed user's guide which describes the input data required to run the code.

Open PDF

Document Details

Document Type
Technical Report
Publication Date
Jun 01, 1984
Accession Number
ADA328841

Entities

People

  • Roger S. Strawn
  • William S. Kobayashi

Tags

Communities of Interest

  • Advanced Electronics
  • Space
  • Weapons Technologies

DTIC Thesaurus Topics

  • Aerodynamic Heating
  • Boundary Layer
  • Energy Transfer
  • Flow
  • Fluid Flow
  • Geometry
  • Heat Energy
  • Heat Of Fusion
  • Heat Transfer
  • Laminar Flow
  • Mach Number
  • Supersonic Flow
  • Swept Wings
  • Thermal Conductivity
  • Thermodynamics
  • Turbulent Flow
  • Two Dimensional

Fields of Study

  • Physics

Readers

  • Aerodynamics/Aeronautics.
  • Combustion and Flow Dynamics.
  • Computer Science.

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Flow