H. L. Runyan

859 total citations
37 papers, 613 citations indexed

About

H. L. Runyan is a scholar working on Aerospace Engineering, Computational Mechanics and Environmental Engineering. According to data from OpenAlex, H. L. Runyan has authored 37 papers receiving a total of 613 indexed citations (citations by other indexed papers that have themselves been cited), including 28 papers in Aerospace Engineering, 26 papers in Computational Mechanics and 4 papers in Environmental Engineering. Recurrent topics in H. L. Runyan's work include Computational Fluid Dynamics and Aerodynamics (16 papers), Fluid Dynamics and Turbulent Flows (13 papers) and Aeroelasticity and Vibration Control (7 papers). H. L. Runyan is often cited by papers focused on Computational Fluid Dynamics and Aerodynamics (16 papers), Fluid Dynamics and Turbulent Flows (13 papers) and Aeroelasticity and Vibration Control (7 papers). H. L. Runyan collaborates with scholars based in United States and Russia. H. L. Runyan's co-authors include Donald S. Woolston, Robert E. Andrews, Charles E Watkins, W Hayes, Harvey H. Hubbard, W. H. Reed, Xue‐Cheng Tai, H. J. Cunningham, J. S. Mixson and C. E. Hammond and has published in prestigious journals such as The Journal of the Acoustical Society of America, Journal of Sound and Vibration and Journal of Aircraft.

In The Last Decade

H. L. Runyan

32 papers receiving 554 citations

Peers

H. L. Runyan
R. L. Bisplinghoff United States
GARABED ZARTARIAN United States
Donald S. Woolston United States
I. E. Garrick United States
G. Alvin Pierce United States
G. H. Gaonkar United States
John C. Houbolt United States
E. D. Albano United States
F. Sisto United States
W. H. Reed United States
R. L. Bisplinghoff United States
H. L. Runyan
Citations per year, relative to H. L. Runyan H. L. Runyan (= 1×) peers R. L. Bisplinghoff

Countries citing papers authored by H. L. Runyan

Since Specialization
Citations

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

Fields of papers citing papers by H. L. Runyan

Since Specialization
Physical SciencesHealth SciencesLife SciencesSocial Sciences

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

Co-authorship network of co-authors of H. L. Runyan

This figure shows the co-authorship network connecting the top 25 collaborators of H. L. Runyan. A scholar is included among the top collaborators of H. L. Runyan 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 H. L. Runyan. H. L. Runyan 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.
Runyan, H. L., et al.. (1985). Application of a lifting surface theory for a helicopter in forward flight. 4 indexed citations
2.
Reed, W. H., et al.. (1980). Decoupler Pylon: A Simple, Effective Wing/Store Flutter Suppressor. Journal of Aircraft. 17(3). 206–211. 28 indexed citations
3.
Hayes, W & H. L. Runyan. (1972). Sonic-Boom Propagation through a Stratified Atmosphere. The Journal of the Acoustical Society of America. 51(2C). 695–701. 28 indexed citations
4.
Hubbard, Harvey H., et al.. (1971). A review of rotating blade noise technology. Journal of Sound and Vibration. 19(3). 227–249. 28 indexed citations
5.
Maglieri, Domenic J., et al.. (1971). Measured and calculated sonic boom signatures from six nonaxisymmetric wind tunnel models. NASA Technical Reports Server (NASA). 255. 341.
6.
Hayes, W & H. L. Runyan. (1970). Propagation of sonic boom through a stratified atmosphere. NASA Technical Reports Server (NASA). 3 indexed citations
7.
Hubbard, Harvey H., et al.. (1970). A review of rotating blade noise technology. NASA Technical Reports Server (NASA). 1 indexed citations
8.
Runyan, H. L., et al.. (1968). Evaluation of certain minimum boom concepts. NASA Technical Reports Server (NASA). 1 indexed citations
9.
Runyan, H. L.. (1968). Some Recent Information on Aircraft Vibration Due to Aerodynamic Sources. The Journal of the Acoustical Society of America. 44(1_Supplement). 364–364. 1 indexed citations
10.
Runyan, H. L., et al.. (1961). Flutter at Very High Speeds. NASA Technical Reports Server (NASA). 3 indexed citations
11.
Runyan, H. L., et al.. (1958). Effect of aerodynamic heating on the flutter of a rectangular wing at a Mach number of 2. University of North Texas Digital Library (University of North Texas). 12 indexed citations
12.
Runyan, H. L., et al.. (1958). Theoretical Considerations of Flutter at High Mach Numbers. Journal of the aerospace sciences. 25(6). 371–381. 33 indexed citations
13.
Runyan, H. L. & Donald S. Woolston. (1956). Method for calculating the aerodynamic loading on an oscillating finite wing in subsonic and sonic flow. University of North Texas Digital Library (University of North Texas). 15 indexed citations
14.
Runyan, H. L., et al.. (1956). Theoretical and experimental investigation of the effect of tunnel walls on the forces on an oscillating airfoil in two-dimensional subsonic compressible flow. University of North Texas Digital Library (University of North Texas). 19 indexed citations
15.
Watkins, Charles E, H. L. Runyan, & Donald S. Woolston. (1955). On the Kernel Function of the Integral Equation Relating the Lift and Downwash Distributions of Oscillating Finite Wings in Subsonic Flow. University of North Texas Digital Library (University of North Texas). 62 indexed citations
16.
Woolston, Donald S. & H. L. Runyan. (1955). Some Considerations on the Air Forces on a Wing Oscillating Between Two Walls for Subsonic Compressible Flow. Journal of the aeronautical sciences. [REQUEST TITLE]. 22(1). 41–50. 18 indexed citations
17.
Woolston, Donald S., et al.. (1955). Some effects of system nonlinearities in the problem of aircraft flutter. University of North Texas Digital Library (University of North Texas). 43 indexed citations
18.
Runyan, H. L., et al.. (1953). A theoretical and experimental study of wind-tunnel-wall effects on oscillating air forces for two-dimensional subsonic compressible flow. NASA Technical Reports Server (NASA). 1 indexed citations
19.
Runyan, H. L.. (1952). Single-degree-of-freedom-flutter calculations for a wing in subsonic potential flow and comparison with an experiment. University of North Texas Digital Library (University of North Texas). 15 indexed citations
20.
Runyan, H. L. & Charles E Watkins. (1951). Considerations on the effect of wind-tunnel walls on oscillating air forces for two-dimensional subsonic compressible flow. University of North Texas Digital Library (University of North Texas). 16 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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