HEATED ANNULI COMPUTER PROGRAM
Technical Report
·
OSTI ID:4837980
The problem analysis and IBM 704 computing techniques for the determination of the aerothermodynamic performance of GE-ANPD concentric-ring- type fuel elements are presented. This program, known as the heated annuli program, will predict exit bulk fluid and ring temperatures, pressure drop, and flow distribution in each annulus of a multistage concentric-ring-type fuel cartridge. The formulation and coding of this problem was set up for air as the fluid being heated. With slight modifications, however, the gas. (auth)
- Research Organization:
- General Electric Co. Flight Propulsion Lab. Dept., Cincinnati
- DOE Contract Number:
- AF33(600)-38062; AND AT(11-1)-171
- NSA Number:
- NSA-15-032288
- OSTI ID:
- 4837980
- Report Number(s):
- APEX-627
- Resource Relation:
- Other Information: Orig. Receipt Date: 31-DEC-61
- Country of Publication:
- United States
- Language:
- English
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