NEA-0802 OWEN-1.
OWEN-1, LOCA Transient and Steady-State 2 Phase Flow in Heated Channel
NAME OR DESIGNATION OF PROGRAM,
COMPUTER,
NATURE OF PHYSICAL PROBLEM SOLVED,
METHOD OF SOLUTION,
RESTRICTIONS ON THE COMPLEXITY OF THE PROBLEM,
TYPICAL RUNNING TIME,
UNUSUAL FEATURES OF THE PROGRAM,
RELATED AND AUXILIARY PROGRAMS,
STATUS,
REFERENCES,
MACHINE REQUIREMENTS,
LANGUAGE,
OPERATING SYSTEM OR MONITOR UNDER WHICH PROGRAM IS EXECUTED,
OTHER RESTRICTIONS,
NAME AND ESTABLISHMENT OF AUTHOR,
MATERIAL,
CATEGORIES
1. NAME OR DESIGNATION OF PROGRAM: OWEN-1.
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| Program name |
Package id |
Status |
Status date |
| OWEN-1 |
NEA-0802/01 |
Tested |
01-SEP-1976 |
Machines used:
| Package ID |
Orig. computer |
Test computer |
| NEA-0802/01 |
IBM 370 series |
IBM 370 series |
3. NATURE OF PHYSICAL PROBLEM SOLVED
The transient (including LOCA) and steady state flow of two-phase compressible light water in a single heated channel. The momentum flux term is included and unequal phase velocities are allowed. A lumped fuel model and detailed surface transfer are included. Thermodynamic equilibrium of the two phases is assumed at each axial location. Either Fauske or Moody choke flow model may be used.
4. METHOD OF SOLUTION
The one-dimensional conservation equations of mass, momentum and energy are solved by a numerically stable implicit finite difference scheme.
5. RESTRICTIONS ON THE COMPLEXITY OF THE PROBLEM
Maximum of 50 axial nodes. There is one lumped fuel node at each axial node.
6. TYPICAL RUNNING TIME
A blowdown problem with 25 nodes takes about two minutes on an IBM 360/65.
7. UNUSUAL FEATURES OF THE PROGRAM
The numerical scheme is stable for all time step sizes so the time step size can be chosen on accuracy considerations alone giving much shorter computation times. Unequal phase velocities are allowed giving a more accurate representation.
8. RELATED AND AUXILIARY PROGRAMS
The equation of state tables have been generated by the ASTEM (ANCR-1026) code.
| Package ID |
Status date |
Status |
| NEA-0802/01 |
01-SEP-1976 |
Tested at NEADB |
10. REFERENCES
- W.J. Turner:
AAEC/E342 (1975)
- W.J. Turner:
Energia Nucleare 19 (5) 317 (1972)
11. MACHINE REQUIREMENTS: 224k bytes main storage; on-line punch and printer; clock.
12. PROGRAMMING LANGUAGE(S) USED
| Package ID |
Computer language |
| NEA-0802/01 |
FORTRAN+ASSEMBLER |
13. OPERATING SYSTEM OR MONITOR UNDER WHICH PROGRAM IS EXECUTED: IBM360 OS MVT.
14. OTHER PROGRAMMING OR OPERATING INFORMATION OR RESTRICTIONS
ANY OTHER PROGRAMMING OR OPERATING INFORMATION OR RESTRICTIONS
15. NAME AND ESTABLISHMENT OF AUTHOR
W.J. Turner:
Australian Atomic Energy Commission Research Establishment
Private Mail Bag
Sutherland, N.S.W. 2232
Australia
NEA-0802/01
| File name |
File description |
Records |
| NEA0802_01.001 |
INFORMATION |
16 |
| NEA0802_01.002 |
SOURCE PROGRAM (F4) EBCDIC |
1870 |
| NEA0802_01.003 |
SOURCE PROGRAM (ASSEMBLER) EBCDIC |
46 |
| NEA0802_01.004 |
DD CARDS + SAMPLE PROBLEM INPUT DATA |
49 |
| NEA0802_01.005 |
LIBRARY DATA (BINARY) |
57 |
| NEA0802_01.006 |
SAMPLE PRINTED OUTPUT (THROUGH UNIT 3) |
249 |
| NEA0802_01.007 |
SAMPLE PRINTED OUTPUT (THROUGH UNIT 10) |
47 |
| NEA0802_01.008 |
SAMPLE PROBLEM PUNCHED OUTPUT |
29 |
- H. Heat Transfer and Fluid Flow
Keywords: blowdown, compressible flow, finite difference method, heat transfer, loss-of-coolant accident, transients, two-phase flow.