Low speed, two-phase, incompressible jet flows

Author(s):  
T. Mautner
Keyword(s):  
Energies ◽  
2021 ◽  
Vol 14 (16) ◽  
pp. 5063
Author(s):  
Norbert Zöbinger ◽  
Thorsten Schweizer ◽  
Thomas Lauer ◽  
Heiko Kubach ◽  
Thomas Koch

The root cause of the initial low-speed pre-ignition (LSPI) is not yet clarified. The literature data suggest that a two-phase phenomenon is most likely triggering the unpredictable premature ignitions in highly boosted spark-ignition engines. However, there are different hypotheses regarding the actual initiator, whether it is a detached liquid oil-fuel droplet or a solid-like particle from deposits. Therefore, the present work investigates the possibility of oil droplet-induced pre-ignitions using a modern downsized engine with minimally invasive endoscopic optical accessibility incorporating in-cylinder lubrication oil detection via light-induced fluorescence. This setup enables the differentiation between liquid and solid particles. Furthermore, the potential of hot solid particles to initiate an ignition under engine-relevant conditions is analyzed numerically. To do so, the particle is generalized as a hot surface transferring heat to the reactive ambient gas phase. The gas-phase reactivity is represented as a TRF/air mixture based on RON/MON specifications of the investigated fuel. The chemical processes are predicted using a semi-detailed reaction mechanism, including 137 species and 633 reactions in a 2D CFD simulation framework. In the optical experiments, no evidence of a liquid oil droplet-induced pre-ignition could be found. Nevertheless, all observed pre-ignitions had a history of flying light-emitting objects. There are strong hints towards solid-like deposit LSPI initiation. The application of the numerical methodology to mean in-cylinder conditions of an LSPI prone engine operation point reveals that particles below 1000 K are not able to initiate a pre-ignition. A sensitivity analysis of the thermodynamic boundary conditions showed that the particle temperature is the most decisive parameter on the calculated ignition delay time.


Author(s):  
Timothy S. Andreychek ◽  
Maurice E. Dingler ◽  
John DeBarba ◽  
William F. Sadowski

A postulated Loss-of-Coolant Accident (LOCA) for a Pressurized Water Reactor (PWR) results in the escape of high-pressure, high-temperature subcooled coolant from the pipe break location. As the coolant escapes from the break, it forms a two-phase jet. The impingement of a two-phase jet may damage protective coatings used on surfaces inside the reactor containment building, resulting in the generation of coatings debris. The coatings debris may be transported to the pool forming on the containment floor. When the Emergency Core Cooling (ECC) and the Containment Spray (CS) Systems are realigned to draw suction from the containment sump, the coatings debris can be transported to the containment sump screen. Large amounts of coatings debris at the sump screen may contribute to undesirable head losses across the sump screen and have undesirable effects on components downstream of the screen. This paper presents the experimental program undertaken to study the performance of Design Basis Accident (DBA) Qualified/Acceptable coating systems typically used inside PWR containments under jet impingement loads, temperatures and pressures associated with a postulated large break LOCA. The coating systems were applied to both carbon steel and concrete substrates consistent with the manner in which the coating systems were applied for DBA testing. A total of eight (8) coupons were subjected to the thermal and hydraulic processes and phenomena associated with jet impingement that would result from the coatings being in close proximity to a postulated large break LOCA. A description of the test protocol, the test facility, and the test conditions is presented, along with post-test inspection summaries for the individual test coupons. This paper will also discuss the extension of the test data to other DBA Qualified/Acceptable epoxy coating systems and untopcoated IOZ coating systems.


2017 ◽  
Vol 52 (1) ◽  
pp. 128-137 ◽  
Author(s):  
N. A. Baryshnikov ◽  
G. V. Belyakov ◽  
S. B. Turuntaev

1987 ◽  
Vol 53 (1) ◽  
pp. 763-767
Author(s):  
�. I. Vitkin ◽  
L. T. Perel'man ◽  
Yu. V. Khodyko

1984 ◽  
Vol 20 (3) ◽  
pp. 330-334 ◽  
Author(s):  
V. V. Andreev ◽  
A. P. Ershov ◽  
L. A. Luk'yanchikov
Keyword(s):  

1998 ◽  
Vol 20 (2) ◽  
pp. 37-45
Author(s):  
Hoang Duc Lien ◽  
I. S. Antonov ◽  
Nguyen Thanh Nam

A modification of k-ε turbulent model is described with application to the numerical investigation of two-phase turbulent jets. In difference of existed two-parameter models, new three-parameter modification have been suggested. In this case an additional equation for transportation of turbulent energy of admixture – kP is used together with equations of transportation of carrier-phase turbulent energy – kg and its dissipation - ε. Additional dissipation terms in the above mentioned equations are defined in connection with a new examination of the between-phases interaction forces determining jet flows.


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