A. M. Cary

422 total citations
27 papers, 344 citations indexed

About

A. M. Cary is a scholar working on Computational Mechanics, Aerospace Engineering and Mechanical Engineering. According to data from OpenAlex, A. M. Cary has authored 27 papers receiving a total of 344 indexed citations (citations by other indexed papers that have themselves been cited), including 24 papers in Computational Mechanics, 16 papers in Aerospace Engineering and 9 papers in Mechanical Engineering. Recurrent topics in A. M. Cary's work include Fluid Dynamics and Turbulent Flows (22 papers), Computational Fluid Dynamics and Aerodynamics (13 papers) and Heat Transfer Mechanisms (8 papers). A. M. Cary is often cited by papers focused on Fluid Dynamics and Turbulent Flows (22 papers), Computational Fluid Dynamics and Aerodynamics (13 papers) and Heat Transfer Mechanisms (8 papers). A. M. Cary collaborates with scholars based in United States. A. M. Cary's co-authors include J. N. Hefner, M. H. Bertram, Dennis M. Bushnell, W. D. Harvey, J. B. Anders, P. C. Stainback, Leonard M. Weinstein, J. E. Harris, D. BUSHNELL and David R. Stone and has published in prestigious journals such as AIAA Journal, Journal of Heat Transfer and Journal of Spacecraft and Rockets.

In The Last Decade

A. M. Cary

27 papers receiving 308 citations

Peers

A. M. Cary
Raymond Sedney United States
W. D. Harvey United States
G. G. Mateer United States
M. H. Bertram United States
J. M. Allen United States
R. E. Melnik United States
BARRY L. REEVES United States
L. S. King United States
M. Inouye United States
Josef Rom Israel
Raymond Sedney United States
A. M. Cary
Citations per year, relative to A. M. Cary A. M. Cary (= 1×) peers Raymond Sedney

Countries citing papers authored by A. M. Cary

Since Specialization
Citations

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

Fields of papers citing papers by A. M. Cary

Since Specialization
Physical SciencesHealth SciencesLife SciencesSocial Sciences

This network shows the impact of papers produced by A. M. Cary. 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 A. M. Cary. The network helps show where A. M. Cary may publish in the future.

Co-authorship network of co-authors of A. M. Cary

This figure shows the co-authorship network connecting the top 25 collaborators of A. M. Cary. A scholar is included among the top collaborators of A. M. Cary 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 A. M. Cary. A. M. Cary 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.
Cary, A. M., et al.. (1986). The optimum hypersonic wind tunnel. 12 indexed citations
2.
Cary, A. M., Dennis M. Bushnell, & J. N. Hefner. (1979). Predicted Effects of Tangential Slot Injection on Turbulent Boundary Layer Flow over a Wide Speed Range. Journal of Heat Transfer. 101(4). 699–704. 8 indexed citations
3.
Hefner, J. N., A. M. Cary, & D. BUSHNELL. (1977). DOWNSTREAM INFLUENCE OF SWEPT SLOT INJECTION IN HYPERSONIC TURBULENT FLOW. NASA STI/Recon Technical Report N. 77. 29452. 1 indexed citations
4.
Bushnell, Dennis M., A. M. Cary, & J. E. Harris. (1976). Calculation methods for compressible turbulent boundary layers. NASA Technical Reports Server (NASA). 78. 13371. 13 indexed citations
5.
Harvey, W. D., A. M. Cary, & J. E. Harris. (1975). Experimental and numerical investigation of boundary-layer development and transition on the walls of a Mach 5 nozzle. NASA STI/Recon Technical Report N. 76. 12315. 2 indexed citations
6.
Hefner, J. N., A. M. Cary, & D. BUSHNELL. (1974). Investigation of the three-dimensional turbulent flow downstream of swept slot injection in hypersonic flow. 5 indexed citations
7.
Cary, A. M. & M. H. Bertram. (1974). Engineering prediction of turbulent skin friction and heat transfer in high-speed flow. NASA Technical Reports Server (NASA). 17 indexed citations
8.
9.
Cary, A. M. & J. N. Hefner. (1972). Film-Cooling Effectiveness and Skin Friction in Hypersonic Turbulent Flow. AIAA Journal. 10(9). 1188–1193. 76 indexed citations
10.
11.
Cary, A. M.. (1970). Turbulent-boundary-layer heat-transfer and transition measurements with surface cooling at Mach 6. NASA Technical Reports Server (NASA). 7 indexed citations
12.
Stone, David R., et al.. (1970). Use of discrete sonic jets as boundary-layer trips in hypersonic flow. AIAA Journal. 8(5). 945–947. 7 indexed citations
13.
Cary, A. M.. (1970). Summary of available information on Reynolds analogy for zero-pressure-gradient, compressible, turbulent-boundary-layer flow. NASA Technical Reports Server (NASA). 20 indexed citations
14.
Cary, A. M. & J. N. Hefner. (1970). Film cooling effectiveness in hypersonic turbulent flow. AIAA Journal. 8(11). 2090–2091. 35 indexed citations
15.
Cary, A. M., et al.. (1969). Downstream Effects of Boundary Layer Trips in Hypersonic Flow. NASA Special Publication. 216. 437. 7 indexed citations
16.
Cary, A. M.. (1968). Turbulent boundary-layer heat transfer and transition measurements for cold-wall conditions at Mach 6.. AIAA Journal. 6(5). 958–959. 16 indexed citations
17.
Cary, A. M., et al.. (1967). Transformation of hypersonic turbulent boundary layers to incompressible form.. AIAA Journal. 5(6). 1202–1203. 3 indexed citations
18.
Bertram, M. H., et al.. (1967). Heat transfer to wavy wall in hypersonic flow.. AIAA Journal. 5(10). 1760–1767. 21 indexed citations
19.
Bertram, M. H., et al.. (1967). Effect of two-dimensional multiple-wave distortions on the heat transfer to a wall in hypersonic flow.. NASA Technical Reports Server (NASA). 4 indexed citations
20.
Cary, A. M., et al.. (1965). A parametric study of the aerodynamic charac- teristics of nose-cylinder-flare bodies at a mach number of 6.0. NASA Technical Reports Server (NASA). 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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