Pan et al 2021a - Revision history

937409527pj at 08:48, 13 December 2021

2021-12-13T08:48:43Z

937409527pj: Minor revision

2021-12-13T08:24:44Z

Minor revision

937409527pj: Minor revision

2021-12-13T07:58:57Z

Minor revision

Rimni: /* Acknowledgments */

2021-12-09T12:36:04Z

‎Acknowledgments

Rimni: /* 3.4 Effect of ice crystals on compressor efficiency */

2021-12-09T12:28:08Z

‎3.4 Effect of ice crystals on compressor efficiency

Rimni at 12:07, 9 December 2021

2021-12-09T12:07:18Z

937409527pj at 03:37, 8 December 2021

2021-12-08T03:37:14Z

937409527pj at 03:34, 8 December 2021

2021-12-08T03:34:38Z

Rimni at 13:44, 3 December 2021

2021-12-03T13:44:42Z

Rimni at 13:00, 3 December 2021

2021-12-03T13:00:08Z

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 |  style="text-align: center;font-size: 75%;"|(a) Particle temperature
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 |  style="text-align: center;font-size: 75%;"|(b) Particle diameter

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 |  style="text-align: center;font-size: 75%;"|(a) Static temperature

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 ==Acknowledgments==
-The authors wish to acknowledge the financial support for this work by Open Fund of Key Laboratory of Icing and Anti/De-icing (Grant NO. IADL20190306), Key research projects of Civil Aviation Flight University of China (Grant NO. ZJ2019-02) and Student Science and Technology Innovation Fund Project（Grant NO.X2021-5).
+The authors wish to acknowledge the financial support for this work by Open Fund of Key Laboratory of Icing and Anti/De-icing (Grant NO. IADL20190306), Key research projects of Civil Aviation Flight University of China (Grant NO. ZJ2019-02) and Student Science and Technology Innovation Fund Project (Grant NO.X2021-5).
 ==References==

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-| <math>\mbox{W}_\mbox{v}=C_{\mbox{p,v}}T_{\mbox{t1}}\left[{\left(\frac{p_{\mbox{t2}}}{p_{\mbox{t1}}}\right)}^{\frac{k_\mbox{v}\mbox{-1}}{k_\mbox{v}}}\mbox{-1}\right]</math>
+| <math>W_\mbox{v}=C_{\mbox{p,v}}T_{\mbox{t1}}\left[{\left(\frac{p_{\mbox{t2}}}{p_{\mbox{t1}}}\right)}^{\frac{k_\mbox{v}\mbox{-1}}{k_\mbox{v}}}\mbox{-1}\right]</math>
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 | style="width: 5px;text-align: right;white-space: nowrap;" | (28)

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 The aviation industry found that a number of engine power-loss events were related to the ice crystal icing, and the research on ice crystal icing had gradually attracted the attention of scholars. In this work, the compressor and ice crystals ingested are regarded as study objects, and the trajectories of particles are calculated based on the Lagrangian approach. Moreover, the two-way coupling method is applied to solve the heat and mass transfer process between ice crystals and the flow field. The variation of particle diameter and temperature under different MVD (Medium Volume Diameter), RH (Relative Humidity) and TWC (Total Water Contents), and the variation of temperature, velocity and pressure of internal flow field are also studied. The result indicates that the MVD, RH and TWC play an important role in the ice crystals motion. Moreover, the temperature and velocity of internal flow field are also greatly affected by the three parameters while the pressure is little affected. In addition, without considering the ice crystal icing, the ice crystals ingested by the compressor would reduce the total temperature at the outlet of compressor, and improve the isentropic efficiency and mass flow rate.
-'''Keywords'''：Ice crystal icing, particle trajectory, compressor, numerical simulation
+'''Keywords''': Ice crystal icing, particle trajectory, compressor, numerical simulation
 ==1. Introduction==

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 The authors wish to acknowledge the financial support for this work by Open Fund of Key Laboratory of Icing and Anti/De-icing (Grant NO. IADL20190306) and Key research projects of Civil Aviation Flight University of China (Grant NO. ZJ2019-02).
-==Reference==
+==References==
-[1] Bravin M., Strapp J., Mason J. An Investigation into Location and Convective Lifecycle Trends in an Ice Crystal Icing Engine Event Database. SAE Technical Paper, 2015.
+[1] Bravin M., Strapp J., Mason J. An investigation into location and convective lifecycle trends in an ice crystal icing engine event database. SAE Technical Paper 2015-01-2130, 2015.
-[2] Mason J.G., Strapp W., Chow P. The Ice Particle Threat to Engines in Flight. 44th AIAA Aerospace Sciences Meeting and Exhibit, 2006.
+[2] Mason J.G., Strapp W., Chow P. The ice particle threat to engines in flight. 44th AIAA Aerospace Sciences Meeting and Exhibit, 9-12 January, Reno, Nevada, 2006.
-[3] Mason J.G., Chow P., Fuleki D.M. Understanding Ice Crystal Accretion and Shedding Phenomenon in Jet Engines Using a Rig Test. Journal of Engineering for Gas Turbines & Power, 133(4): 041201, 2011.
+[3] Mason J.G., Chow P., Fuleki D.M. Understanding ice crystal accretion and shedding phenomenon in jet engines using a rig test. Journal of Engineering for Gas Turbines & Power, 133(4):041201, 2011.
-[4] Veres J., Jorgenson P., Wright W. A Model to Assess the Risk of Ice Accretion due to Ice Crystal Ingestion in a Turbofan Engine and its Effects on Performance. 4th AIAA Atmospheric and Space Environments Conference, 2012.
+[4] Veres J., Jorgenson P., Wright W. A model to assess the risk of ice accretion due to ice crystal ingestion in a turbofan engine and its effects on performance. 4th AIAA Atmospheric and Space Environments Conference, 25-28 June, New Orleans, Louisiana, 2012.
-[5] Struk P., Currie T., Wright W., Knezevici D. Fundamental Ice Crystal Accretion Physics Studies. SAE Technical Paper, 2011-38-0018, 2011.
+[5] Struk P., Currie T., Wright W., Knezevici D. Fundamental ice crystal accretion physics studies. SAE Technical Paper, 2011-38-0018, 2011.
-[6] Kott B., Struk P. M., Bartkus T. P. A Study of Ice-Crystal Icing Erosion Using the NASA Icing Research Tunnel and Propulsion Systems Laboratory. AIAA AVIATION 2020 FORUM, 2020.
+[6] Kott B., Struk P.M., Bartkus T.P. A study of ice-crystal icing erosion using the NASA icing research tunnel and propulsion systems laboratory. AIAA AVIATION 2020 FORUM, June 15-19, 2020.
-[7] Struk P. M., Tsao J.C., Bartkus T.P. Plans and Preliminary Results of Fundamental Studies of Ice Crystal Icing Physics in the NASA Propulsion Systems Laboratory. 8th AIAA Atmospheric and Space Environments Conference, AIAA 2016-3738, 2016.
+[7] Struk P.M., Tsao J.C., Bartkus T.P. Plans and preliminary results of fundamental studies of ice crystal icing physics in the NASA propulsion systems laboratory. 8th AIAA Atmospheric and Space Environments Conference, AIAA 2016-3738, 2016.
 [8] Baumert A., Bansmer S.E., Bacher M. Implementation of an innovative ice crystal generation system to the Icing Wind Tunnel Braunschweig. 53rd AIAA Aerospace Sciences Meeting, AIAA 2015-1225, 2015.
-[9] Baumert A., Bansmer S., Trontin P., Villedieu P. Experimental and numerical investigations on aircraft icing at mixed phase conditions. International Journal of Heat and Mass Transfer, 123(aug.):957-78, 2018.
+[9] Baumert A., Bansmer S., Trontin P., Villedieu P. Experimental and numerical investigations on aircraft icing at mixed phase conditions. International Journal of Heat and Mass Transfer, 123:957-78, 2018.
 [10] Villedieu P, Trontin P, Chauvin R. Glaciated and mixed phase ice accretion modeling using ONERA 2D icing suite. 6th AIAA Atmospheric and Space Environments Conference, 2014.

← Older revision		Revision as of 13:00, 3 December 2021
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	The authors wish to acknowledge the financial support for this work by Open Fund of Key Laboratory of Icing and Anti/De-icing (Grant NO. IADL20190306) and Key research projects of Civil Aviation Flight University of China (Grant NO. ZJ2019-02).		The authors wish to acknowledge the financial support for this work by Open Fund of Key Laboratory of Icing and Anti/De-icing (Grant NO. IADL20190306) and Key research projects of Civil Aviation Flight University of China (Grant NO. ZJ2019-02).
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	==Reference==		==Reference==