INVESTIGATION OF TURBULENT HEAT TRANSFER AT HYPERSONIC SPEEDS. VOLUME III. THE LAMINAR-TURBULENT RHO SUB R MU SUB R MOMENTUM INTEGRAL AND TURBULENT NONSIMILAR BOUNDARY LAYER COMPUTER PROGRAMS
Abstract
The report presents a combined analytical and experimental investigation of turbulent heat transfer on basic and composite configurations at hypersonic speeds. Computer programs incorporating the analytical methods described are presented in Volume III. The two heat-transfer prediction methods programmed are the laminar-turbulent rho sub r mu sub r momentum integral method and the turbulent nonsimilar method. This volume of the report describes the numerical method and presents flow charts, program listings, input forms, and a description of the output for each program. The programs are written in Fortran IV language for operation on the IBM 7094.
Document Details
- Document Type
- Technical Report
- Publication Date
- Dec 01, 1967
- Accession Number
- AD0667804
Entities
People
- Carl L. Jaeck
- James R. Mitchell
- Richard T. Savage
Organizations
- Boeing