Accession Number:

AD0749482

Title:

Aerospace Synthesized Aerodynamic Heating Program

Descriptive Note:

Rept. for Jul 1963-Apr 1971

Corporate Author:

AEROSPACE CORP SAN BERNARDINO CA SAN BERNARDINO OPERATIONS

Report Date:

1972-03-15

Pagination or Media Count:

208.0

Abstract:

The Aerospace Synthesized Aerodynamic Heating Program is written in the Fortran 4 language for the IBM-360-65 computer. This program calculates heating and internal conduction for shapes approximating those of missiles. To do this, it couples various correlations for external high speed convective aerodynamic, for nonaerodynamic, heating with internal transient heat conduction and surface ablation. These may be applied to flat plates, wedges, cones, sphere-cones, spheres, or cylinders with laminar andor turbulent heat transfer equations applied to the configurations listed. The method is sufficiently general to allow many variations in the physical properties of materials and boundary conditions that one might wish to consider.

Subject Categories:

  • Guided Missile Dynamics, Configurations and Control Surfaces
  • Fluid Mechanics

Distribution Statement:

APPROVED FOR PUBLIC RELEASE