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Francis J. Capone

Observed names: Capone, F. J., F. CAPONE, F. J. Capone, FRANCIS CAPONE, Francis Capone, Francis-J. Capone
OpenAlex ID: A5111847406
The nonaxisymmetric nozzle - It is for real
1979 · F. J. Capone · NASA Technical Reports Server (NASA) · 40
Free-To-Roll Analysis of Abrupt Wing Stall on Military Aircraft at Transonic Speeds
2003 · Bruce Owens, Francis Capone, et al. · AIAA Aerospace Sciences Meeting and Exhibit · 38
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Transonic Free-to-Roll Analysis of Abrupt Wing Stall on Military Aircraft
2004 · D. B. Owens, Francis J. Capone, et al. · Journal of Aircraft · 32
AWS Figure of Merit (FOM) Developed Parameters from Static, Transonic Model Tests
2003 · John Lamar, Francis Capone, et al. · AIAA Aerospace Sciences Meeting and Exhibit · 32
Enhancements to the FAST-MAC Circulation Control Model and Recent High-Reynolds Number Testing in the National Transonic Facility
2013 · William E. Milholen, Gregory S. Jones, et al. · AIAA Applied Aerodynamics Conference · 30
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High-alpha vectoring characteristics of the F-18/HARV
1994 · Scott C. Asbury, Francis J. Capone · Journal of Propulsion and Power · 27
Static internal performance of an axisymmetric nozzle with multiaxis thrust-vectoring capability
1991 · George T. Carson, F. J. Capone · University of Michigan Library Repository · 22
Data reduction formulas for the 16-foot transonic tunnel: NASA Langley Research Center, revision 2
1992 · C. E. Mercer, B. L. Berrier, et al. · NASA Technical Reports Server (NASA) · 21
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Development of the Circulation Control Flow Scheme used in the NTF Semi-Span FAST-MAC Model
2013 · Gregory S. Jones, William E. Milholen, et al. · AIAA Applied Aerodynamics Conference · 20
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Development of a Transonic Free-To-Roll Test Capability
2004 · Francis J. Capone, D. Bruce Owens, et al. · Journal of Aircraft · 19
Development of a Free-To-Roll Transonic Test Capability
2003 · Francis Capone, D. Bruce Owens, et al. · AIAA Aerospace Sciences Meeting and Exhibit · 19
The NASA Langley 16-Foot Transonic Tunnel---Historical Overview, Facility Description, Calibration, Flow Characteristics, Test Capabilities
1995 · F. J. Capone, Linda S. Bangert, et al. · NASA Technical Reports Server (NASA) · 19
Static performance of five twin-engine nonaxisymmetric nozzles with vectoring and reversing capability
1978 · F. J. Capone · NASA STI Repository (National Aeronautics and Space Administration) · 19
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Experimental determination of equivalent solid bodies to represent jets exhausting into a Mach 2.20 external stream
1969 · F. J. Capone, L. E. Putnam · University of Michigan Library Repository · 19
Recommended Experimental Procedures for Evaluation of Abrupt Wing Stall Characteristics
2003 · Francis Capone, Robert Hall, et al. · AIAA Aerospace Sciences Meeting and Exhibit · 17
Static Performance of Vectoring/Reversing Nonaxisymmetric Nozzles
1979 · C.M. Willard, F. J. Capone, et al. · Journal of Aircraft · 17
Comparative investigation of multiplane thrust vectoring nozzles
1992 · F. CAPONE, P. SMERECZNIAK, et al. · AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit · 16
Summary of Propulsive-Lift Research in the Langley 16-Ft Transonic Tunnel
1976 · Francis-J. Capone · Journal of Aircraft · 14
Supercirculation Effects Induced by Vectoring a Partial-Span Rectangular Jet
1975 · Francis J. Capone · Journal of Aircraft · 14
Study of External Dynamic Flap Loads on a 6 Percent B-1B Model
1992 · J. M. Seiner, J. C. Manning, et al. · Journal of Engineering for Gas Turbines and Power · 13
Reduction of wind-tunnel-model vibration by means of a tuned damped vibration absorber installed in the model
1968 · F. J. Capone, W. B. Igoe · NASA Technical Reports Server (NASA) · 13
Liftoff and Transition Aerodynamics of the Ares I Launch Vehicle
2012 · Francis J. Capone, John W. Paulson, et al. · Journal of Spacecraft and Rockets · 11
Review and Recommended Experimental Procedures For Evaluation Of Abrupt Wing Stall Characteristics
2004 · Francis J. Capone, Robert M. Hall, et al. · Journal of Aircraft · 11
Performance characteristics of two multiaxis thrust-vectoring nozzles at Mach numbers up to 1.28
1993 · David J. Wing, F. J. Capone · NASA Technical Reports Server (NASA) · 11
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Static internal performance of convergent single-expansion-ramp nozzles with various combinations of internal geometric parameters
1989 · E. A. Bare, F. J. Capone · NASA STI Repository (National Aeronautics and Space Administration) · 11
Works count: 98
Citation count: 729
H-index: 16
I10-index: 30
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