Ashvin Hosangadi

1.6k citations
120 papers · 1.3k indexed · h-index 17
Topics
Computational Fluid Dynamics and Aerodynamics (42 papers)Rocket and propulsion systems research (37 papers)Spacecraft and Cryogenic Technologies (26 papers)

In The Last Decade

Ashvin Hosangadi

109 papers receiving 1.1k citations

Peers

Ashvin Hosangadi
Comparison fields: 5 of 52
  • Computational Mechanics 775
  • Aerospace Engineering 745
  • Mechanics of Materials 481
  • Mechanical Engineering 358
  • Applied Mathematics 120
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Citations per field
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Citations per year

Countries citing papers authored by Ashvin Hosangadi

Since Specialization
Citations

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

Fields of papers citing papers by Ashvin Hosangadi

Since Specialization
Physical SciencesHealth SciencesLife SciencesSocial Sciences

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

Co-authorship network of co-authors of Ashvin Hosangadi

This figure shows the co-authorship network connecting the top 25 collaborators of Ashvin Hosangadi. A scholar is included among the top collaborators of Ashvin Hosangadi 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 Ashvin Hosangadi. Ashvin Hosangadi 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
#WorkIndexed citations
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2 0
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8 11
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Computational Analyses in Support of Sub-scale Diffuser Testing for the A-3 Facility
4
10 29
11 13
12 7
13 7
14
A Generalized Multi-Phase Framework for Modeling Cavitation in Cryogenic Fluids
4
15 6
16 27
17
Recent developments in the simulation of steady and transient transverse jet interactions for missile, rotorcraft, and propulsive applications
5
18 5
19 13
20 1

About Ashvin Hosangadi

Ashvin Hosangadi is a scholar working on Computational Mechanics, Aerospace Engineering and Applied Mathematics, having authored 120 papers that have together received 1.3k indexed citations. Recurring topics across this work include Computational Fluid Dynamics and Aerodynamics (42 papers), Rocket and propulsion systems research (37 papers) and Spacecraft and Cryogenic Technologies (26 papers). The work is most often cited by research in Computational Mechanics (775 citations), Aerospace Engineering (745 citations) and Mechanics of Materials (481 citations). Ashvin Hosangadi has collaborated with scholars based in United States, Russia and Poland. Frequent co-authors include Vineet Ahuja, Srinivasan Arunajatesan, Neeraj Sinha, Peter Cavallo, B. YORK, Sukanta Dash, Sanford Dash, Zisen Liu, Robert Lee and Yu-Tai Lee. Their work appears in journals such as International Journal of Heat and Mass Transfer, Chemical Engineering Science and AIAA Journal.

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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