Accession Number : ADA328841

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

Descriptive Note : Final rept.,

Corporate Author : ACUREX CORP/AEROTHERM MOUNTAIN VIEW CA

Personal Author(s) : Strawn, Roger S. ; Kobayashi, William S.

PDF Url : ADA328841

Report Date : JUN 1984

Pagination or Media Count : 87

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.

Descriptors :   *COMPUTERIZED SIMULATION, *PROJECTILES, *SWEPT WINGS, *CONDUCTION(HEAT TRANSFER), *AERODYNAMIC HEATING, PROGRAMMING MANUALS, COMPUTATIONS, GRIDS, FINITE DIFFERENCE THEORY, DIFFERENTIAL EQUATIONS, THERMAL RESISTANCE, BOUNDARY LAYER FLOW, HEAT OF FUSION.

Subject Categories : Ammunition and Explosives

Distribution Statement : APPROVED FOR PUBLIC RELEASE