Countries citing papers authored by E. Carson Yates
Since
Specialization
Citations
This map shows the geographic impact of E. Carson Yates'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 E. Carson Yates with the expected number of citations based on a country's size and research output (numbers larger than one mean the country cites E. Carson Yates more than expected).
This network shows the impact of papers produced by E. Carson Yates. 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 E. Carson Yates. The network helps show where E. Carson Yates may publish in the future.
Co-authorship network of co-authors of E. Carson Yates
This figure shows the co-authorship network connecting the top 25 collaborators of E. Carson Yates.
A scholar is included among the top collaborators of E. Carson Yates 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 E. Carson Yates. E. Carson Yates 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.
Yates, E. Carson. (1989). AGARD standard aeroelastic configurations for dynamic response. NASA STI Repository (National Aeronautics and Space Administration).57 indexed citations
2.
Yates, E. Carson. (1987). Aerodynamic sensitivities from subsonic, sonic and supersonic unsteady, nonplanar lifting-surface theory. NASA Technical Reports Server (NASA).24 indexed citations
3.
Yates, E. Carson. (1985). Unsteady transonic flows - Introduction, current trends, applications. NASA Technical Reports Server (NASA).2 indexed citations
4.
Yates, E. Carson. (1985). Unsteady subsonic and supersonic flows - Historical review; state of the art. NASA Technical Reports Server (NASA).3 indexed citations
Bland, Samuel R. & E. Carson Yates. (1963). Comparative evaluation of methods for predicting flutter and divergence of unswept wings of finite span. NASA Technical Reports Server (NASA).3 indexed citations
19.
Yates, E. Carson, et al.. (1963). Steady-state characteristics of a differential -pressure system for evaluating angles of attack and sideslip of the ranger iv vehicle. NASA Technical Reports Server (NASA).2 indexed citations
20.
Yates, E. Carson. (1960). USE OF EXPERIMENTAL STEADY-FLOW AERODYNAMIC PARAMETERS IN THE CALCULATION OF FLUTTER CHARACTERISTICS FOR FINITE-SPAN SWEPT ON UNSWEPT WINGS AT SUBSONIC, TRANSONIC, AND SUPERSONIC SPEEDS. NASA Technical Reports Server (NASA).7 indexed citations
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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
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