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Home | Products | PIPESTRESS | Thermal Transients | Transient Stresses
TRANSIENT STRESSES
Stresses due to thermal transients are documented in PIPESTRESS report F-1, shown below.
D S T C O M P U T E R S E R V I C E S S. A. G E N E V A F-1 PAGE NO. 216 - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - ++ DST/PIPESTRESS ++ NUCLEAR POWER PLANT S. BOONE Version 3.5.0+417 PC Release: Sep 1999 - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - CALCULATION NUMBER 3999 CODE SECTION III CLASS 1 ASME-1977 TEST PROBLEM NO. 1 2001/01/15 14:36:18 [261] CLASS 1 ANALYSIS FATIGUE PROTECTION INCLUDING STATIC AND SEISMIC LOADS, AND TRANSIENT LOADING CASE NO. 82 TRANSIENT ANALYSIS - THERMAL TRANSIENT 66 DELTA T IN DEGREES F STRESSES IN PSI =========== EQUATION 10 ========== ============== EQUATION 11 ============== ======= EQUATION 13 ======= POINT TIME DELTA STRESS TIME DELTA DELTA STRESS TIME STRESS NO. (SEC) T1 TA TB (SEC) T1 TA TB T2 (SEC) TA TB TANGENT 1 3.26 5.4 662.0 662.0 648. 3.26 5.4 662.0 662.0 1.0 1356. 0.00 0.0 0.0 0. 105 7.79 5.1 658.3 657.1 994. 5.41 5.4 660.2 659.1 1.0 1913. 15.58 652.7 651.4 218. TANGENT 105 7.79 5.1 658.3 657.1 994. 5.41 5.4 660.2 659.1 1.0 1913. 15.58 652.7 651.4 218. 2 3.26 5.4 662.0 662.0 648. 3.26 5.4 662.0 662.0 1.0 1356. 0.00 0.0 0.0 0. REDUCER 2 3.26 5.4 662.0 662.0 648. 3.26 5.4 662.0 662.0 1.0 1356. 0.00 0.0 0.0 0. 2 3.26 5.4 662.0 662.0 648. 3.26 5.4 662.0 662.0 1.0 902. 0.00 0.0 0.0 0. 3 9.27 3.8 662.0 662.0 454. 9.27 3.8 662.0 662.0 0.7 622. 0.00 0.0 0.0 0. 3 9.27 3.8 662.0 662.0 454. 9.27 3.8 662.0 662.0 0.7 1017. 0.00 0.0 0.0 0. TANGENT 3 9.27 3.8 662.0 662.0 454. 9.27 3.8 662.0 662.0 0.7 1017. 0.00 0.0 0.0 0. 4 9.27 3.8 662.0 662.0 454. 9.27 3.8 662.0 662.0 0.7 1017. 0.00 0.0 0.0 0. LR ELBOW 4 9.27 3.8 662.0 662.0 454. 9.27 3.8 662.0 662.0 0.7 1017. 0.00 0.0 0.0 0. 4 9.27 3.8 662.0 662.0 454. 9.27 3.8 662.0 662.0 0.7 667. 0.00 0.0 0.0 0. 5 9.27 3.8 662.0 662.0 454. 9.27 3.8 662.0 662.0 0.7 667. 0.00 0.0 0.0 0. 5 9.27 3.8 662.0 662.0 454. 9.27 3.8 662.0 662.0 0.7 1017. 0.00 0.0 0.0 0. TANGENT 5 9.27 3.8 662.0 662.0 454. 9.27 3.8 662.0 662.0 0.7 1017. 0.00 0.0 0.0 0. 6 9.27 3.8 662.0 662.0 454. 9.27 3.8 662.0 662.0 0.7 667. 0.00 0.0 0.0 0. TANGENT 6 9.27 3.8 662.0 662.0 454. 9.27 3.8 662.0 662.0 0.7 667. 0.00 0.0 0.0 0. 7 9.27 3.8 662.0 662.0 454. 9.27 3.8 662.0 662.0 0.7 1017. 0.00 0.0 0.0 0. REDUCER 7 9.27 3.8 662.0 662.0 454. 9.27 3.8 662.0 662.0 0.7 1017. 0.00 0.0 0.0 0. 7 9.27 3.8 662.0 662.0 454. 9.27 3.8 662.0 662.0 0.7 622. 0.00 0.0 0.0 0. 8 5.34 4.4 662.2 662.2 533. 5.34 4.4 662.2 662.2 0.8 736. 0.00 0.0 0.0 0. 8 5.34 4.4 662.2 662.2 533. 5.34 4.4 662.2 662.2 0.8 1110. 0.00 0.0 0.0 0. LR ELBOW 8 5.34 4.4 662.2 662.2 533. 5.34 4.4 662.2 662.2 0.8 1110. 0.00 0.0 0.0 0. 8 5.34 4.4 662.2 662.2 533. 5.34 4.4 662.2 662.2 0.8 736. 0.00 0.0 0.0 0. 9 5.34 4.4 662.2 662.2 533. 5.34 4.4 662.2 662.2 0.8 736. 0.00 0.0 0.0 0. 9 5.34 4.4 662.2 662.2 533. 5.34 4.4 662.2 662.2 0.8 1110. 0.00 0.0 0.0 0. TANGENT 9 5.34 4.4 662.2 662.2 533. 5.34 4.4 662.2 662.2 0.8 1110. 0.00 0.0 0.0 0. 10 43.04 2.9 647.2 629.1 3416. 43.04 2.9 647.2 629.1 0.5 3543. 43.04 647.2 629.1 1531. TANGENT 10 43.04 2.9 647.2 629.1 3416. 43.04 2.9 647.2 629.1 0.5 3543. 43.04 647.2 629.1 1531. 11 5.34 4.4 662.2 662.2 533. 5.34 4.4 662.2 662.2 0.8 1110. 0.00 0.0 0.0 0. LR ELBOW 11 5.34 4.4 662.2 662.2 533. 5.34 4.4 662.2 662.2 0.8 1110. 0.00 0.0 0.0 0. 11 5.34 4.4 662.2 662.2 533. 5.34 4.4 662.2 662.2 0.8 736. 0.00 0.0 0.0 0. 12 5.34 4.4 662.2 662.2 533. 5.34 4.4 662.2 662.2 0.8 736. 0.00 0.0 0.0 0. 12 5.34 4.4 662.2 662.2 533. 5.34 4.4 662.2 662.2 0.8 1110. 0.00 0.0 0.0 0. |
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