Chung-Jen Tam - Concepedia

Author

Chung-Jen Tam

Taitech (United States)

Also Known As

Chung-Jen (John) Tam, Chung-Jen Tam, Chung-jen Tam

Publications

1.1K

Citations

H-Index

Concepts

All Affiliations

Taitech (United States)United States Air Force Research Laboratory Wright-Patterson Air Force Base Innovative Scientific Solutions (United States)University of Cincinnati

About

Chung-Jen Tam is an author at Taitech (United States) specializing in engineering, space engineering, and aerodynamics.

Top Concepts

#	Concept	H-Index	Publications	Citations
1	Engineering	19	28	965
2	Mechanical Engineering	11	11	255
3	Natural Sciences	2	2	65
4	Health Sciences	1	1	21
5	Mechanics	1	1	24

Chung-Jen Tam

Publications

Citations

H-Index

Page 1

	Year	Citations
Plasma-Assisted Ignition in Scramjets Lance Jacobsen, Campbell D. Carter, Thomas Jackson, Journal of Propulsion and Power Planar Laser-induced FluorescenceEngineeringPlasma-assisted IgnitionAerospace EngineeringCombustion Science	2008	123
Cavity ignition in supersonic flow by spark discharge and pulse detonation Timothy Ombrello, Campbell D. Carter, Chung-Jen Tam, Proceedings of the Combustion Institute Cavity IgnitionEngineeringDetonation PhenomenonPulse DetonationPropulsion	2014	85
Design and analysis of streamline traced hypersonic inlets F. S. Billig, Robert A. Baurle, Chung-Jen Tam, 9th International Space Planes and Hypersonic Systems and Technologies Conference Unsteady FlowEngineeringAerospace EngineeringInlet AerodynamicsHypersonic Inlets	1999	84
Flame Characteristics and Fuel Entrainment Inside a Cavity Flame Holder of a Scramjet Combustor Kuo-Cheng Lin, Chung-Jen Tam, Isaac Boxx, EngineeringAerospace EngineeringCombustion ScienceCavity FlameFlame Characteristics	2007	78
Algebraic turbulence model simulations of supersonic open-cavity flow physics Chung-Jen Tam, Paul D. Orkwis, Peter J. Disimile AIAA Journal AeroacousticsVortex DynamicsUnsteady FlowEngineeringAerospace Engineering	1996	71
Starting and Operation of a Streamline-Traced Busemann Inlet at Mach 4 Lance Jacobsen, Chung-Jen Tam, Robert Behdadnia, Mach 4EngineeringFlow ControlStreamline-traced Busemann InletFluid Mechanics	2006	42
Characterization of Shock Train Structures inside Constant-Area Isolators of Model Scramjet Combustors Kuo-Cheng Lin, Chung-Jen Tam, Kevin Jackson, 44th AIAA Aerospace Sciences Meeting and Exhibit Model Scramjet CombustorsShock TrainEngineeringFlow ControlDetonation Phenomenon	2006	41
Shock-Train Structure Resolved with Absorption Spectroscopy Part II: Analysis and CFD Comparison C. D. Lindstrom, D. J. Davis, Skip Williams, AIAA Journal Shock-train Structure ResolvedPhysicsNatural SciencesSpectroscopyAbsorption Spectroscopy	2009	36
Study on the Operability of Cavity Flameholders inside a Scramjet Combustor Kuo-Cheng Lin, Chung-Jen Tam, Kevin Jackson EngineeringAerospace EngineeringCombustion ScienceCombustion EngineeringPresent Flowpath	2009	34
Dual-Mode Scramjet Combustor: Numerical Sensitivity and Evaluation of Experiments Ryan Milligan, Jiwen Liu, Chung-Jen Tam, 50th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition Grid RefinementEngineeringAerospace EngineeringDual-mode Scramjet CombustorCombustion Science	2012	32

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