Ching Y. Loh

920 total citations
48 papers, 591 citations indexed

About

Ching Y. Loh is a scholar working on Computational Mechanics, Aerospace Engineering and Applied Mathematics. According to data from OpenAlex, Ching Y. Loh has authored 48 papers receiving a total of 591 indexed citations (citations by other indexed papers that have themselves been cited), including 46 papers in Computational Mechanics, 26 papers in Aerospace Engineering and 11 papers in Applied Mathematics. Recurrent topics in Ching Y. Loh's work include Computational Fluid Dynamics and Aerodynamics (38 papers), Fluid Dynamics and Turbulent Flows (31 papers) and Aerodynamics and Acoustics in Jet Flows (23 papers). Ching Y. Loh is often cited by papers focused on Computational Fluid Dynamics and Aerodynamics (38 papers), Fluid Dynamics and Turbulent Flows (31 papers) and Aerodynamics and Acoustics in Jet Flows (23 papers). Ching Y. Loh collaborates with scholars based in United States, Canada and Hong Kong. Ching Y. Loh's co-authors include Lennart S. Hultgren, Philip C. E. Jorgenson, K. B. M. Q. Zaman, W. H. Hui, Sin-Chung Chang, Milo D. Dahl, Timothy J. Bencic, James Scott, Sheng‐Tao Yu and H. Rasmussen and has published in prestigious journals such as Journal of Fluid Mechanics, Journal of Computational Physics and International Journal of Heat and Mass Transfer.

In The Last Decade

Ching Y. Loh

44 papers receiving 558 citations

Peers

Countries citing papers authored by Ching Y. Loh

Since Specialization

Citations

This map shows the geographic impact of Ching Y. Loh'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 Ching Y. Loh with the expected number of citations based on a country's size and research output (numbers larger than one mean the country cites Ching Y. Loh more than expected).

Fields of papers citing papers by Ching Y. Loh

Since Specialization

Physical SciencesHealth SciencesLife SciencesSocial Sciences

This network shows the impact of papers produced by Ching Y. Loh. 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 Ching Y. Loh. The network helps show where Ching Y. Loh may publish in the future.

Co-authorship network of co-authors of Ching Y. Loh

This figure shows the co-authorship network connecting the top 25 collaborators of Ching Y. Loh. A scholar is included among the top collaborators of Ching Y. Loh 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 Ching Y. Loh. Ching Y. Loh is excluded from the visualization to improve readability, since they are connected to all nodes in the network.

All Works

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20 of 20 papers shown

#	Work	Indexed citations
1	An exactly force-balanced boundary-conforming arbitrary-Lagrangian-Eulerian method for interfacial dynamics 2020 ·Journal of Computational Physics ·(unknown), Jie Li, Ching Y. Loh, Li‐Shi Luo	10
2	Towards An 'All Speed' Unstructured Upwind Scheme 2009 ·NASA STI Repository (National Aeronautics and Space Administration) ·Ching Y. Loh, Philip C. E. Jorgenson	1
3	Multi-dimensional dissipation for cure of pathological behaviors of upwind scheme 2008 ·Journal of Computational Physics ·Ching Y. Loh, Philip C. E. Jorgenson	14
4	A Time-accurate Upwind Unstructured Finite volume Method for Compressible Flow with Cure of Pathological Behaviors 2007 ·NASA STI Repository (National Aeronautics and Space Administration) ·Ching Y. Loh, Philip C. E. Jorgenson	7
5	Computation of Tone Noise from Supersonic Jet Impinging on Flat Plates 2005 ·43rd AIAA Aerospace Sciences Meeting and Exhibit ·Ching Y. Loh	9
6	A Robust Absorbing Boundary Condition for Compressible Flows 2005 ·NASA Technical Reports Server (NASA) ·Ching Y. Loh, Philip C. E. Jorgenson	6
7	Computation of Jet Screech Noise 2003 ·Lennart S. Hultgren, Ching Y. Loh	1
8	A 3-D CE/SE Navier-Stokes Solver with Unstructured Hexahedral Grid for Computation of Nearfield Jet Screech Noise 2003 ·NASA STI Repository (National Aeronautics and Space Administration) ·Ching Y. Loh, (unknown), Lennart S. Hultgren	21
9	On a Non-Reflecting Boundary Condition for Hyperbolic Conservation Laws 2003 ·Ching Y. Loh	11
10	Numerical investigation of 'transonic resonance' with a convergent-divergent nozzle 2002 ·K. B. M. Q. Zaman, Ching Y. Loh	5
11	Computing Axisymmetric Jet Screech Tones using Unstructured Grids 2002 ·NASA Technical Reports Server (NASA) ·Philip C. E. Jorgenson, Ching Y. Loh	21
12	Near field screech noise computation for an underexpanded supersonic jet by the CE/SE method 2001 ·NASA Technical Reports Server (NASA) ·Ching Y. Loh, Lennart S. Hultgren, Philip C. E. Jorgenson	18
13	Wave computation in compressible flow using space-time conservation element and solution element method 2001 ·AIAA Journal ·Ching Y. Loh, Lennart S. Hultgren, Sin-Chung Chang	1
14	Robust and simple non-reflecting boundary conditions for the space-time conservation element and solution element method 1997 ·Sin-Chung Chang, Ching Y. Loh, Sheng‐Tao Yu, (unknown), Xiao-Yen Wang, Philip C. E. Jorgenson, (unknown)	33
15	The space-time conservation element method - A new numerical scheme for computational aeroacoustics 1996 ·34th Aerospace Sciences Meeting and Exhibit ·Ching Y. Loh, (unknown), James Scott, Sheng‐Tao Yu	15
16	Computational aeroacoustics via the space-time conservation element/solution element method 1996 ·Ching Y. Loh, (unknown), James Scott	12
17	Theoretical study of the incompressible Navier-Stokes equations by the least-squares method 1994 ·NASA Technical Reports Server (NASA) ·Bo‐nan Jiang, Ching Y. Loh, Louis A. Povinelli	11
18	Three-dimensional steady supersonic duct flow using Lagrangian formulation 1994 ·Shock Waves ·Ching Y. Loh, Meng‐Sing Liou	4
19	Computing 3-D steady supersonic flow via a new Lagrangian approach 1993 ·31st Aerospace Sciences Meeting ·Ching Y. Loh, Meng‐Sing Liou	2
20	A new Lagrangian method for steady supersonic flow computation part II. Slip-line resolution 1992 ·Journal of Computational Physics ·W. H. Hui, Ching Y. Loh	19

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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