Diganta Narzary

738 total citations
31 papers, 590 citations indexed

About

Diganta Narzary is a scholar working on Mechanical Engineering, Aerospace Engineering and Computational Mechanics. According to data from OpenAlex, Diganta Narzary has authored 31 papers receiving a total of 590 indexed citations (citations by other indexed papers that have themselves been cited), including 30 papers in Mechanical Engineering, 29 papers in Aerospace Engineering and 19 papers in Computational Mechanics. Recurrent topics in Diganta Narzary's work include Turbomachinery Performance and Optimization (29 papers), Heat Transfer Mechanisms (24 papers) and Tribology and Lubrication Engineering (11 papers). Diganta Narzary is often cited by papers focused on Turbomachinery Performance and Optimization (29 papers), Heat Transfer Mechanisms (24 papers) and Tribology and Lubrication Engineering (11 papers). Diganta Narzary collaborates with scholars based in United States and Mexico. Diganta Narzary's co-authors include Je-Chin Han, Zhihong Gao, Shantanu Mhetras, Akhilesh P. Rallabandi, Srinath V. Ekkad, Junsheng Feng, J. C. Han, Mary Anne Alvin, Jianmei Feng and R. P. Roy and has published in prestigious journals such as International Journal of Heat and Mass Transfer, Journal of Turbomachinery and Journal of Engineering for Gas Turbines and Power.

In The Last Decade

Diganta Narzary

29 papers receiving 579 citations

Peers — A (Enhanced Table)

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

Name h Career Trend Papers Cites
Diganta Narzary United States 13 561 545 444 14 13 31 590
Shantanu Mhetras United States 14 525 0.9× 521 1.0× 412 0.9× 16 1.1× 5 0.4× 29 570
Jaeyong Ahn United States 9 419 0.7× 387 0.7× 326 0.7× 15 1.1× 14 1.1× 11 454
A. J. Rawlinson United Kingdom 14 659 1.2× 624 1.1× 540 1.2× 38 2.7× 18 1.4× 22 719
Hee-Koo Moon United States 13 394 0.7× 388 0.7× 396 0.9× 9 0.6× 9 0.7× 37 485
S. J. Gallimore United Kingdom 10 496 0.9× 316 0.6× 323 0.7× 7 0.5× 16 1.2× 20 528
Heeyoon Chung South Korea 12 226 0.4× 294 0.5× 223 0.5× 20 1.4× 11 0.8× 32 339
Luca Innocenti Italy 11 211 0.4× 279 0.5× 183 0.4× 10 0.7× 12 0.9× 48 324
Isabelle Trébinjac France 13 416 0.7× 298 0.5× 350 0.8× 12 0.9× 40 3.1× 55 460
Michael Fox United States 13 395 0.7× 452 0.8× 423 1.0× 42 3.0× 7 0.5× 51 552
Christian Saumweber Germany 14 798 1.4× 762 1.4× 709 1.6× 13 0.9× 4 0.3× 20 840

Countries citing papers authored by Diganta Narzary

Since Specialization
Citations

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

Fields of papers citing papers by Diganta Narzary

Since Specialization
Physical SciencesHealth SciencesLife SciencesSocial Sciences

This network shows the impact of papers produced by Diganta Narzary. 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 Diganta Narzary. The network helps show where Diganta Narzary may publish in the future.

Co-authorship network of co-authors of Diganta Narzary

This figure shows the co-authorship network connecting the top 25 collaborators of Diganta Narzary. A scholar is included among the top collaborators of Diganta Narzary 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 Diganta Narzary. Diganta Narzary 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.
Narzary, Diganta, et al.. (2016). Film Cooling Performance of Tripod Antivortex Injection Holes Over the Pressure and Suction Surfaces of a Nozzle Guide Vane. Journal of Thermal Science and Engineering Applications. 9(2). 19 indexed citations
2.
Narzary, Diganta, et al.. (2014). Turbine Blade Tip Film-Cooling and Heat Transfer Measurements at High Blowing Ratios. 8 indexed citations
3.
Narzary, Diganta, et al.. (2013). Film-Cooling Performance of Antivortex Hole on a Flat Plate. Journal of Turbomachinery. 135(6). 22 indexed citations
4.
Narzary, Diganta, et al.. (2012). Influence of Coolant Density on Turbine Blade Platform Film-Cooling. Journal of Thermal Science and Engineering Applications. 4(2). 5 indexed citations
5.
Narzary, Diganta, et al.. (2011). Influence of Coolant Density on Turbine Blade Film-Cooling Using Pressure Sensitive Paint Technique. Journal of Turbomachinery. 134(3). 70 indexed citations
6.
Narzary, Diganta. (2010). Experimental Study of Gas Turbine Blade Film Cooling and Heat Transfer. OakTrust (Texas A&M University Libraries). 6 indexed citations
7.
Narzary, Diganta, et al.. (2010). Influence of Coolant Density on Turbine Blade Film-Cooling Using Pressure Sensitive Paint Technique. Volume 4: Heat Transfer, Parts A and B. 1529–1540. 4 indexed citations
8.
Gao, Zhihong, Diganta Narzary, Shantanu Mhetras, & Je-Chin Han. (2009). Effect of Inlet Flow Angle on Gas Turbine Blade Tip Film Cooling. Journal of Turbomachinery. 131(3). 21 indexed citations
9.
Narzary, Diganta, et al.. (2009). Influence of Coolant Density on Turbine Blade Platform Film-Cooling. 287–299. 7 indexed citations
10.
Sierra, Fernando, et al.. (2009). Heat Transfer and Thermal Mechanical Stress Distributions in Gas Turbine Blades. 115–126. 8 indexed citations
11.
Gao, Zhihong, Diganta Narzary, & Je-Chin Han. (2009). Turbine Blade Platform Film Cooling With Typical Stator-Rotor Purge Flow and Discrete-Hole Film Cooling. Journal of Turbomachinery. 131(4). 42 indexed citations
12.
Mhetras, Shantanu, Diganta Narzary, Zhihong Gao, & Je-Chin Han. (2008). Effect of a Cutback Squealer and Cavity Depth on Film-Cooling Effectiveness on a Gas Turbine Blade Tip. Journal of Turbomachinery. 130(2). 56 indexed citations
13.
Gao, Zhihong, Diganta Narzary, & Je-Chin Han. (2008). Film-Cooling on a Gas Turbine Blade Pressure Side or Suction Side With Compound Angle Shaped Holes. Journal of Turbomachinery. 131(1). 48 indexed citations
14.
Gao, Zhihong, Diganta Narzary, Shantanu Mhetras, & Je-Chin Han. (2008). Full-Coverage Film Cooling for a Turbine Blade with Axial-Shaped Holes. Journal of Thermophysics and Heat Transfer. 22(1). 50–61. 25 indexed citations
15.
Sierra, Fernando, et al.. (2008). Influence of Cooling Flow Rate Variation on Gas Turbine Blade Temperature Distributions. Volume 4: Heat Transfer, Parts A and B. 45–53. 7 indexed citations
16.
Gao, Zhihong, Diganta Narzary, Shantanu Mhetras, & Je-Chin Han. (2007). Full Coverage Film Cooling for a Turbine Blade with Axial Shaped Holes. 2 indexed citations
17.
Gao, Zhihong, Diganta Narzary, & Je-Chin Han. (2007). Film-Cooling on a Gas Turbine Blade Pressure Side or Suction Side With Compound Angle Shaped Holes. 569–579. 8 indexed citations
18.
Mhetras, Shantanu, Diganta Narzary, Zhihong Gao, & Je-Chin Han. (2006). Effect of a Cutback Squealer and Cavity Depth on Film-Cooling Effectiveness for a Gas Turbine Blade Tip. 5 indexed citations
19.
Feng, Junsheng, et al.. (2005). Experiment on Gas Ingestion Through Axial-Flow Turbine Rim Seals. Journal of Engineering for Gas Turbines and Power. 127(3). 573–582. 22 indexed citations
20.
Narzary, Diganta, et al.. (2005). Ingestion into a Rotor-Stator Disk Cavity with Single- and Double-Rim Seals. 2 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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