Stephen H Maslen

555 total citations
22 papers, 378 citations indexed

About

Stephen H Maslen is a scholar working on Computational Mechanics, Applied Mathematics and Aerospace Engineering. According to data from OpenAlex, Stephen H Maslen has authored 22 papers receiving a total of 378 indexed citations (citations by other indexed papers that have themselves been cited), including 16 papers in Computational Mechanics, 7 papers in Applied Mathematics and 6 papers in Aerospace Engineering. Recurrent topics in Stephen H Maslen's work include Computational Fluid Dynamics and Aerodynamics (9 papers), Fluid Dynamics and Turbulent Flows (8 papers) and Gas Dynamics and Kinetic Theory (7 papers). Stephen H Maslen is often cited by papers focused on Computational Fluid Dynamics and Aerodynamics (9 papers), Fluid Dynamics and Turbulent Flows (8 papers) and Gas Dynamics and Kinetic Theory (7 papers). Stephen H Maslen collaborates with scholars based in United States and Canada. Stephen H Maslen's co-authors include F. K. Moore, W E Moeckel, S. Ostrach and Maurice E. Tucker and has published in prestigious journals such as AIAA Journal, Journal of Spacecraft and Rockets and Quarterly of Applied Mathematics.

In The Last Decade

Stephen H Maslen

19 papers receiving 341 citations

Peers

Stephen H Maslen
Comparison fields: 5 of 49
  • Computational Mechanics 215
  • Aerospace Engineering 159
  • Applied Mathematics 158
  • Mechanical Engineering 46
  • Biomedical Engineering 45
Replace R. E. Sheer with:
R. E. Sheer United States
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R. E. Sheer United States View profile →
Citations per field, relative to Stephen H Maslen
Stephen H Maslen · 1×
Citations per year, relative to Stephen H Maslen
Stephen H Maslen · 1×

Countries citing papers authored by Stephen H Maslen

Since Specialization
Citations

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

Fields of papers citing papers by Stephen H Maslen

Since Specialization
Physical SciencesHealth SciencesLife SciencesSocial Sciences

This network shows the impact of papers produced by Stephen H Maslen. 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 Stephen H Maslen. The network helps show where Stephen H Maslen may publish in the future.

Co-authorship network of co-authors of Stephen H Maslen

This figure shows the co-authorship network connecting the top 25 collaborators of Stephen H Maslen. A scholar is included among the top collaborators of Stephen H Maslen 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 Stephen H Maslen. Stephen H Maslen 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
# Work Indexed citations
1
Development of a method of analysis and computer program for calculating the inviscid flow about the windward surfaces of space shuttle configurations at large angles of attack
0
2 8
3 2
4 75
5 26
6
STABILITY OF LAMINAR VISCOUS FLOWS WITH A BODY FORCE
4
7
The Magnetic Field of a Finite Solenoid
51
8 6
9 11
10 58
11 17
12 1
13
SATELLITE AND SPACE PROPULSION SYSTEMS
1
14 55
15
Transverse oscillations in a cylindrical combustion chamber
6
16
Second approximation to laminar compressible boundary layer on flat plate in slip flow
17
17
Three-Dimensional Supersonic Nozzles and Inlets of Arbitrary Exit Cross Section
6
18
Supersonic conical flow
8
19
Turbulent boundary-layer temperature recovery factors in two-dimensional supersonic flow
4
20
Experimental Pressure Distributions over Two Wing-body Combinations at Mach Number 1.9
1

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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