F. G. Moore

417 total citations
60 papers, 278 citations indexed

About

F. G. Moore is a scholar working on Aerospace Engineering, Computational Mechanics and Applied Mathematics. According to data from OpenAlex, F. G. Moore has authored 60 papers receiving a total of 278 indexed citations (citations by other indexed papers that have themselves been cited), including 48 papers in Aerospace Engineering, 31 papers in Computational Mechanics and 11 papers in Applied Mathematics. Recurrent topics in F. G. Moore's work include Computational Fluid Dynamics and Aerodynamics (31 papers), Rocket and propulsion systems research (24 papers) and Aerospace and Aviation Technology (21 papers). F. G. Moore is often cited by papers focused on Computational Fluid Dynamics and Aerodynamics (31 papers), Rocket and propulsion systems research (24 papers) and Aerospace and Aviation Technology (21 papers). F. G. Moore collaborates with scholars based in United States. F. G. Moore's co-authors include Floyd J. Wilcox, R. C. Swanson, Fred R. DeJarnette, Lee E. Moore, Jinjing Sun, J. L. Frierson and William W. Hager and has published in prestigious journals such as AIAA Journal, Journal of Aircraft and Journal of Spacecraft and Rockets.

In The Last Decade

F. G. Moore

53 papers receiving 221 citations

Peers — A (Enhanced Table)

Peers by citation overlap · career bar shows stage (early→late) cites · hero ref

Name	h						Papers	Cites
F. G. Moore United States	9	237	165	75	19	18	60	278
A. R. Seebass United States	9	141 0.6×	229 1.4×	81 1.1×	7 0.4×	9 0.5×	29	273
Thino Eggers Germany	12	250 1.1×	219 1.3×	154 2.1×	21 1.1×	10 0.6×	44	329
Harry E. Bailey United States	9	105 0.4×	199 1.2×	94 1.3×	14 0.7×	7 0.4×	19	259
D. Caruana France	11	435 1.8×	374 2.3×	32 0.4×	10 0.5×	10 0.6×	18	482
Sidra I. Silton United States	12	341 1.4×	342 2.1×	105 1.4×	8 0.4×	22 1.2×	46	428
Josef Rom Israel	10	237 1.0×	284 1.7×	83 1.1×	5 0.3×	11 0.6×	42	362
JOHN ANDERSON United States	9	152 0.6×	188 1.1×	151 2.0×	19 1.0×	4 0.2×	17	323
Walter B. Sturek United States	13	271 1.1×	426 2.6×	103 1.4×	15 0.8×	13 0.7×	54	479
Jose Caram United States	9	160 0.7×	165 1.0×	134 1.8×	43 2.3×	7 0.4×	20	269
B. J. GRIFFITH United States	10	155 0.7×	168 1.0×	167 2.2×	31 1.6×	5 0.3×	28	268

Countries citing papers authored by F. G. Moore

Since Specialization

Citations

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

Fields of papers citing papers by F. G. Moore

Since Specialization

Physical SciencesHealth SciencesLife SciencesSocial Sciences

This network shows the impact of papers produced by F. G. Moore. 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 F. G. Moore. The network helps show where F. G. Moore may publish in the future.

Co-authorship network of co-authors of F. G. Moore

This figure shows the co-authorship network connecting the top 25 collaborators of F. G. Moore. A scholar is included among the top collaborators of F. G. Moore 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 F. G. Moore. F. G. Moore is excluded from the visualization to improve readability, since they are connected to all nodes in the network.

All Works

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20 of 20 papers shown

Moore, F. G., et al.. (2010). Improvements to Power-On Base Pressure Prediction for the Aeroprediction Code. 48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition. 1 indexed citations

Moore, F. G., et al.. (2008). New Methods to Predict Nonlinear Pitch Damping Moments. 46th AIAA Aerospace Sciences Meeting and Exhibit. 2 indexed citations

Moore, F. G., et al.. (2008). New Methods to Predict Nonlinear Pitch Damping Moments. Journal of Spacecraft and Rockets. 45(3). 495–503. 4 indexed citations

Moore, F. G., et al.. (2004). An Approximate Method to Estimate Wing Trailing-Edge Bluntness Effects on Normal Force. 42nd AIAA Aerospace Sciences Meeting and Exhibit. 1 indexed citations

Moore, F. G., et al.. (2004). 2002 Version of the Aeroprediction Code (AP02). Journal of Spacecraft and Rockets. 41(2). 232–247. 1 indexed citations

Moore, F. G., et al.. (2002). The 2002 Version of the Aeroprediction Code. Part 1. Summary of New Theoretical Methodology. Defense Technical Information Center (DTIC). 1 indexed citations

Moore, F. G., et al.. (2001). Improved Power-On, Base Drag Methodology for the Aeroprediction Code. Defense Technical Information Center (DTIC). 4 indexed citations

Moore, F. G.. (2000). Approximate Methods for Weapon Aerodynamics. American Institute of Aeronautics and Astronautics, Inc. eBooks. 47 indexed citations

Moore, F. G., et al.. (1998). Improved Methodology for Axial Force Prediction at Angle of Attack. Journal of Spacecraft and Rockets. 35(2). 132–139. 1 indexed citations

10.

Moore, F. G., et al.. (1995). A new method for calculating wing alone aerodynamics to angle of attack 180 degrees. 33rd Aerospace Sciences Meeting and Exhibit. 2 indexed citations

11.

Moore, F. G., et al.. (1994). Base drag prediction on missile configurations. Journal of Spacecraft and Rockets. 31(5). 759–765. 10 indexed citations

12.

Moore, F. G., et al.. (1993). Incorporation of boundary layer heating predictive methodology into NSWCDD aeroprediction code. Defense Technical Information Center (DTIC). 94. 15632.

13.

Moore, F. G., et al.. (1993). New Approximate Method for Calculating Real Gas Effects on Missile Configurations. Journal of Spacecraft and Rockets. 30(1). 22–31. 3 indexed citations

14.

Moore, F. G., et al.. (1992). Second-Order Shock-Expansion Theory Extended to Include Real Gas Effects. Defense Technical Information Center (DTIC). 5 indexed citations

15.

Moore, F. G., et al.. (1992). New Methods for Predicting Nonlinear Lift, Center of Pressure, and Pitching Moment on Missile Configurations.. 5 indexed citations

16.

Moore, F. G. & R. C. Swanson. (1978). Dynamic Derivatives for Missile Configurations to Mach Number Three. Journal of Spacecraft and Rockets. 15(2). 65–66. 15 indexed citations

17.

Frierson, J. L., et al.. (1978). An Electrostatic Roll Sensor for Supersonic Vehicles Part I: Feasibility and Flight Tests. Journal of Aircraft. 15(4). 195–198.

18.

Moore, F. G. & R. C. Swanson. (1977). Aerodynamics of Tactical Weapons to Mach Number 3 and Angle of Attack 15 deg. Part I. Theory and Application.. Defense Technical Information Center (DTIC). 1 indexed citations

19.

Hager, William W., Fred R. DeJarnette, & F. G. Moore. (1977). Optimal Projectile Shapes for Minimum Total Drag. Defense Technical Information Center (DTIC).

20.

Moore, F. G., et al.. (1976). The Effect of Boattail Shape on Magnus,. Defense Technical Information Center (DTIC). 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.

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