K.-C. Lin

680 total citations
22 papers, 557 citations indexed

About

K.-C. Lin is a scholar working on Computational Mechanics, Aerospace Engineering and Electrical and Electronic Engineering. According to data from OpenAlex, K.-C. Lin has authored 22 papers receiving a total of 557 indexed citations (citations by other indexed papers that have themselves been cited), including 18 papers in Computational Mechanics, 6 papers in Aerospace Engineering and 4 papers in Electrical and Electronic Engineering. Recurrent topics in K.-C. Lin's work include Fluid Dynamics and Heat Transfer (12 papers), Combustion and flame dynamics (10 papers) and Fluid Dynamics and Turbulent Flows (6 papers). K.-C. Lin is often cited by papers focused on Fluid Dynamics and Heat Transfer (12 papers), Combustion and flame dynamics (10 papers) and Fluid Dynamics and Turbulent Flows (6 papers). K.-C. Lin collaborates with scholars based in United States, China and South Korea. K.-C. Lin's co-authors include Thomas Jackson, Paul Kennedy, Khaled Sallam, C. D. Carter, Mark Gruber, Jeffrey M. Donbar, Tarun Mathur, F. Billig, G. M. Faeth and Ming‐Chia Lai and has published in prestigious journals such as Engineering Applications of Artificial Intelligence, International Journal for Numerical Methods in Fluids and Combustion Science and Technology.

In The Last Decade

K.-C. Lin

21 papers receiving 544 citations

Peers — A (Enhanced Table)

Peers by citation overlap · career bar shows stage (early→late) cites · hero ref

Name h Career Trend Papers Cites
K.-C. Lin United States 15 455 131 113 90 71 22 557
Prashant Khare United States 14 287 0.6× 150 1.1× 77 0.7× 95 1.1× 27 0.4× 68 474
Mathis Bode Germany 16 461 1.0× 149 1.1× 40 0.4× 35 0.4× 65 0.9× 46 590
Kuo-Cheng Lin United States 21 1.1k 2.4× 602 4.6× 123 1.1× 56 0.6× 68 1.0× 70 1.1k
T. M. Muruganandam India 13 560 1.2× 284 2.2× 52 0.5× 24 0.3× 30 0.4× 57 640
Tongxun Yi United States 12 512 1.1× 155 1.2× 34 0.3× 33 0.4× 18 0.3× 41 562
Pietro Paolo Ciottoli Italy 16 493 1.1× 210 1.6× 59 0.5× 14 0.2× 40 0.6× 53 572
V. Sankaran United States 9 346 0.8× 116 0.9× 26 0.2× 31 0.3× 52 0.7× 16 495
A. L. Kuhl United States 15 228 0.5× 402 3.1× 79 0.7× 13 0.1× 33 0.5× 77 595
Jan Martinez Schramm Germany 15 772 1.7× 547 4.2× 56 0.5× 22 0.2× 57 0.8× 60 915
Vikrant Gupta China 15 429 0.9× 216 1.6× 19 0.2× 33 0.4× 33 0.5× 42 612

Countries citing papers authored by K.-C. Lin

Since Specialization
Citations

This map shows the geographic impact of K.-C. Lin's research. It shows the number of citations coming from papers published by authors working in each country. You can also color the map by specialization and compare the number of citations received by K.-C. Lin with the expected number of citations based on a country's size and research output (numbers larger than one mean the country cites K.-C. Lin more than expected).

Fields of papers citing papers by K.-C. Lin

Since Specialization
Physical SciencesHealth SciencesLife SciencesSocial Sciences

This network shows the impact of papers produced by K.-C. Lin. Nodes represent research fields, and links connect fields that are likely to share authors. Colored nodes show fields that tend to cite the papers produced by K.-C. Lin. The network helps show where K.-C. Lin may publish in the future.

Co-authorship network of co-authors of K.-C. Lin

This figure shows the co-authorship network connecting the top 25 collaborators of K.-C. Lin. A scholar is included among the top collaborators of K.-C. Lin based on the total number of citations received by their joint publications. Widths of edges represent the number of papers authors have co-authored together. Node borders signify the number of papers an author published with K.-C. Lin. K.-C. Lin is excluded from the visualization to improve readability, since they are connected to all nodes in the network.

All Works

20 of 20 papers shown
1.
Wen, Long, et al.. (2023). A new multi-sensor fusion with hybrid Convolutional Neural Network with Wiener model for remaining useful life estimation. Engineering Applications of Artificial Intelligence. 126. 106934–106934. 39 indexed citations
2.
Lin, K.-C., et al.. (2023). Numerical investigation of air curtain jet effect upon the compartment-facade fire safety protection based on temperature evolution and thermal impact. Thermal Science and Engineering Progress. 43. 101988–101988. 18 indexed citations
3.
Sallam, Khaled, et al.. (2014). Digital Holographic Analysis of the Near Field of Aerated-Liquid Jets in Crossflow. Journal of Propulsion and Power. 30(6). 1636–1645. 21 indexed citations
4.
Lin, K.-C., et al.. (2011). Breakup modeling of a liquid jet in cross flow. International Journal of Automotive Technology. 12(4). 489–496. 37 indexed citations
5.
Sheu, Tony W. H., et al.. (2011). Development of a convection–diffusion–reaction model for solving Maxwell's equations in frequency domain. International Journal for Numerical Methods in Fluids. 69(2). 430–441. 1 indexed citations
6.
Sallam, Khaled, et al.. (2009). Spray Structure in Near-Injector Region of Aerated Jet in Subsonic Crossflow. Journal of Propulsion and Power. 25(2). 258–266. 23 indexed citations
7.
Sallam, Khaled, et al.. (2008). Breakup of Aerated Liquid Jets in Subsonic Crossflow. Journal of Propulsion and Power. 24(2). 253–258. 24 indexed citations
8.
Sallam, Khaled, Christian Aalburg, G. M. Faeth, et al.. (2006). PRIMARY BREAKUP OF ROUND AERATED-LIQUID JETS IN SUPERSONIC CROSSFLOWS. Atomization and Sprays. 16(6). 657–672. 45 indexed citations
9.
Williams, Skip, et al.. (2006). Diode Laser Diagnostics of High Speed Flows. 37 indexed citations
10.
Wu, Pei-Kuan, K.-C. Lin, & Thomas Jackson. (2006). Effects of Flow Initial Conditions on Spray Characteristics With and Without Crossflows. 44th AIAA Aerospace Sciences Meeting and Exhibit. 1 indexed citations
11.
Lin, K.-C., et al.. (2005). STRUCTURES AND PHASE TRANSITION PROCESSES OF SUPERCRITICAL METHANE/ETHYLENE MIXTURES INJECTED INTO A SUBCRITICAL ENVIRONMENT. Combustion Science and Technology. 178(1-3). 129–160. 51 indexed citations
12.
Gruber, Mark, et al.. (2005). Structures of Angled Aerated-Liquid Jets in Mach 1.94 Supersonic Crossflow. 43rd AIAA Aerospace Sciences Meeting and Exhibit. 9 indexed citations
13.
Sallam, Khaled, et al.. (2004). Breakup of Aerated-Liquid Jets in Supersonic Crossflows. 42nd AIAA Aerospace Sciences Meeting and Exhibit. 8 indexed citations
14.
Lin, K.-C., Paul Kennedy, & Thomas Jackson. (2002). Penetration heights of liquid jets in high-speed crossflows. 75 indexed citations
15.
Lin, K.-C., Paul Kennedy, & Thomas Jackson. (2001). Structures of aerated-liquid jets in subsonic crossflows. 39th Aerospace Sciences Meeting and Exhibit. 14 indexed citations
16.
Lin, K.-C., Paul Kennedy, & Thomas Jackson. (2001). Structures of internal flow and the corresponding spray for aerated-liquid injectors. 37th Joint Propulsion Conference and Exhibit. 24 indexed citations
17.
Lin, K.-C. & Paul Kennedy. (2000). Spray penetration heights of angle-injected aerated-liquid jets in supersonic crossflows. 38th Aerospace Sciences Meeting and Exhibit. 20 indexed citations
18.
Lin, K.-C., et al.. (2000). Active combustion control for diffusion flames using an integrated fuel injector/flameholder device. 36th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit. 6 indexed citations
19.
Lin, K.-C., Kevin A. Kirkendall, Paul Kennedy, & Thomas Jackson. (1999). Spray structures of aerated liquid fuel jets in supersonic crossflows. 35th Joint Propulsion Conference and Exhibit. 28 indexed citations
20.
Lin, K.-C.. (1986). The gun-launched test for a supersonic parachute. 1 indexed citations

Rankless uses publication and citation data sourced from OpenAlex, an open and comprehensive bibliographic database. While OpenAlex provides broad and valuable coverage of the global research landscape, it—like all bibliographic datasets—has inherent limitations. These include incomplete records, variations in author disambiguation, differences in journal indexing, and delays in data updates. As a result, some metrics and network relationships displayed in Rankless may not fully capture the entirety of a scholar's output or impact.

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