This map shows the geographic impact of C. C. Koch'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 C. C. Koch with the expected number of citations based on a country's size and research output (numbers larger than one mean the country cites C. C. Koch more than expected).
This network shows the impact of papers produced by C. C. Koch. 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 C. C. Koch. The network helps show where C. C. Koch may publish in the future.
Co-authorship network of co-authors of C. C. Koch
This figure shows the co-authorship network connecting the top 25 collaborators of C. C. Koch.
A scholar is included among the top collaborators of C. C. Koch 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 C. C. Koch. C. C. Koch is excluded from
the visualization to improve readability, since they are connected to all nodes in the network.
Koch, C. C., et al.. (1982). Energy efficient engine. High pressure compressor detail design report. NASA Technical Reports Server (NASA).28 indexed citations
Wisler, D. C., C. C. Koch, & L. H. Smith. (1977). Preliminary design study of advanced multistage axial flow core compressors. NASA Technical Reports Server (NASA).6 indexed citations
Koch, C. C. & L. H. Smith. (1976). LOSS SOURCES AND MAGNITUDE IN AXIAL-FLOW COMPRESSORS. 411–424.3 indexed citations
9.
Koch, C. C., et al.. (1972). Evaluation of range and distortion tolerance for high Mach number transonic fan stages. Task 2: Performance of a 1500-foot-per-second tip speed transonic fan stage with variable geometry inlet guide vanes and stator. NASA Technical Reports Server (NASA).1 indexed citations
10.
Koch, C. C., et al.. (1971). Evaluation of range and distortion tolerance for high Mach number transonic fan stages, volume 1 Final report. NASA Technical Reports Server (NASA).1 indexed citations
11.
Koch, C. C.. (1970). Experimental evaluation of outer case blowing or bleeding of single stage axial flow compressor, part 6 Final report. NASA Technical Reports Server (NASA).4 indexed citations
12.
Koch, C. C.. (1969). Experimental evaluation of outer case blowing or bleeding of single stage axial flow compressor. Part 5 - Performance of plain casing insert configuration with distorted inlet flow. NASA STI Repository (National Aeronautics and Space Administration).
13.
Koch, C. C. & L. H. Smith. (1968). Experimental evaluation of outer casing blowing or bleeding of single stage axial flow compressor. Part 2 - Performance of plain casing insert configuration with undistorted inlet flow and boundary layer trip.1 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.