F. J. Capone - Concepedia

Author

F. J. Capone

Langley Research Center

Also Known As

F. CAPONE, F. J. Capone, FRANCIS CAPONE, Francis Capone, Francis J. Capone

Publications

712

Citations

H-Index

Concepts

All Affiliations

Langley Research Center Analytical Mechanics Associates (United States)

About

F. J. Capone is an author at Langley Research Center specializing in aerodynamics, space engineering, and engineering.

Top Concepts

#	Concept	H-Index	Publications	Citations
1	Engineering	16	27	514
2	Computer Engineering	4	4	79
3	Education	2	2	38
4	Health Sciences	2	2	28
5	Kinesiology	2	2	28

F. J. Capone

Publications

535

Citations

H-Index

Page 1

	Year	Citations
The nonaxisymmetric nozzle - It is for real F. J. Capone NASA Technical Reports Server (NASA) Rarefied FlowAeroacousticsCompressible FlowEngineeringAerospace Engineering	1979	39
Free-To-Roll Analysis of Abrupt Wing Stall on Military Aircraft at Transonic Speeds Bruce Owens, F. J. Capone, Robert M. Hall, 41st Aerospace Sciences Meeting and Exhibit AeroacousticsRock DivergenceFree-to-roll AnalysisEngineeringLimit Cycle	2003	38
AWS Figure of Merit (FOM) Developed Parameters from Static, Transonic Model Tests John E. Lamar, F. J. Capone, Robert M. Hall 41st Aerospace Sciences Meeting and Exhibit ReliabilityAlternate FomsReliability EngineeringEngineeringTransonic Model Tests	2003	32
Transonic Free-to-Roll Analysis of Abrupt Wing Stall on Military Aircraft D. Bruce Owens, F. J. Capone, Robert M. Hall, Journal of Aircraft AeroacousticsAeronauticsEngineeringAerospace EngineeringAerospace Simulation	2004	32
High-alpha vectoring characteristics of the F-18/HARV Scott C. Asbury, F. J. Capone Journal of Propulsion and Power EngineeringAerospace EngineeringAerospace SimulationAerospace TechnologyNozzle Pressure Ratios	1994	26
Enhancements to the FAST-MAC Circulation Control Model and Recent High-Reynolds Number Testing in the National Transonic Facility William E. Milholen, Gregory S. Jones, David T. Chan, 31st AIAA Applied Aerodynamics Conference Circulation ControlUnsteady FlowAeronauticsEngineeringFlow Control	2013	26
Data reduction formulas for the 16-foot transonic tunnel: NASA Langley Research Center, revision 2 C. E. Mercer, B. L. Berrier, F. J. Capone, NASA Technical Reports Server (NASA) AeroacousticsEngineeringSkin Friction DragAerospace SimulationWind Engineering	1992	22
Static internal performance of an axisymmetric nozzle with multiaxis thrust-vectoring capability George T. Carson, F. J. Capone NASA Technical Reports Server (NASA) AeroacousticsEngineeringFluid MechanicsMechanical EngineeringAerospace System	1991	22
Static performance of five twin-engine nonaxisymmetric nozzles with vectoring and reversing capability F. J. Capone NASA STI Repository (National Aeronautics and Space Administration) EngineeringAerospace EngineeringTransonic Tunnel TestMechanical EngineeringStatic Performance	1978	20
The NASA Langley 16-Foot Transonic Tunnel---Historical Overview, Facility Description, Calibration, Flow Characteristics, Test Capabilities F. J. Capone, Linda S. Bangert, Scott C. Asbury, NASA Technical Reports Server (NASA) AeroacousticsEngineeringAerospace SimulationAerospace SystemWind Engineering	1995	19

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