Countries citing papers authored by W. D. Grantham
Since
Specialization
Citations
This map shows the geographic impact of W. D. Grantham'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 W. D. Grantham with the expected number of citations based on a country's size and research output (numbers larger than one mean the country cites W. D. Grantham more than expected).
This network shows the impact of papers produced by W. D. Grantham. 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 W. D. Grantham. The network helps show where W. D. Grantham may publish in the future.
Co-authorship network of co-authors of W. D. Grantham
This figure shows the co-authorship network connecting the top 25 collaborators of W. D. Grantham.
A scholar is included among the top collaborators of W. D. Grantham 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 W. D. Grantham. W. D. Grantham is excluded from
the visualization to improve readability, since they are connected to all nodes in the network.
Grantham, W. D.. (1989). Comparison of flying qualities derived from in-flight and ground-based simulators for a jet-transport airplane for the approach and landing pilot tasks. NASA STI Repository (National Aeronautics and Space Administration).8 indexed citations
3.
Grantham, W. D.. (1987). Piloted simulator study of allowable time delays in large-airplane response. NASA Technical Reports Server (NASA). 35(16). 637–42.2 indexed citations
Grantham, W. D., et al.. (1982). Noise and economic characteristics of an advanced blended supersonic transport concept. NASA Technical Reports Server (NASA).2 indexed citations
Grantham, W. D. & Paul M. Smith. (1980). Development of SCR Aircraft takeoff and landing procedures for community noise abatement and their impact on flight safety. NASA STI Repository (National Aeronautics and Space Administration).5 indexed citations
9.
Swift, C.T., W. Linwood Jones, & W. D. Grantham. (1980). Microwave remote sensing. 22(5). 4–9.220 indexed citations
10.
Grantham, W. D., et al.. (1978). Ground-based and in-flight simulator studies of low-speed handling characteristics of two supersonic cruise transport concepts. NASA Technical Reports Server (NASA).1 indexed citations
11.
Grantham, W. D., E. M. Bracalente, W. Linwood Jones, & James W. Johnson. (1977). The SeaSat-A satellite scatterometer. IEEE Journal of Oceanic Engineering. 2(2). 200–206.57 indexed citations
12.
Grantham, W. D., L. T. Nguyen, & P. L. Deal. (1974). Simulation of decelerating landing approaches on an externally blown flap STOL transport airplane. NASA Technical Reports Server (NASA).
13.
Grantham, W. D. & P. L. Deal. (1974). Simulator study of minimum acceptable level of longitudinal stability for a representative STOL configuration during landing approach. NASA STI Repository (National Aeronautics and Space Administration).
14.
Grantham, W. D., et al.. (1972). Fixed base simulator study of an externally blown flap STOL transport airplane during approach and landing. NASA Technical Reports Server (NASA).5 indexed citations
Deal, P. L., et al.. (1970). Simulator study of the instrument landing approach of a heavy subsonic jet transport with an external-flow jet-flap system used for additional lift. NASA Technical Reports Server (NASA).2 indexed citations
17.
Deal, P. L. & W. D. Grantham. (1968). A piloted fixed-base simulator study of low- speed flight characteristics of an arrow-wing supersonic transport design. NASA Technical Reports Server (NASA).2 indexed citations
18.
Grantham, W. D.. (1961). Effects of Mass-Loading Variations and Applied Moments on Motion and Control of a Manned Rotating Space Vehicle. NASA STI Repository (National Aeronautics and Space Administration).2 indexed citations
19.
Bowman, James S. & W. D. Grantham. (1960). Low-Speed Aerodynamic Characteristics of a Model of a Hypersonic Research Airplane at Angles of Attack up to 90 deg for a Range of Reynolds Numbers. NASA Technical Reports Server (NASA).1 indexed citations
20.
Grantham, W. D., et al.. (1960). ANALYTICAL INVESTIGATION AND PREDICTION OF SPIN AND RECOVERY CHARACTERISTICS OF THE NORTH AMERICAN X-15 AIRPLANE. NASA Technical Reports Server (NASA).2 indexed citations
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