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Joseph L. Koncsek

Observed names: J Koncsek, J. KONCSEK, J. Koncsek, J.L. Koncsek, Koncsek, J. L.
OpenAlex ID: A5015634403
Bleed System Design Technology for Supersonic Inlets
1973 · Jan Syberg, Joseph L. Koncsek · Journal of Aircraft · 69
Experimental Evaluation of an Analytically Derived Bleed System for a Supersonic Inlet
1976 · Jan Syberg, Joseph L. Koncsek · Journal of Aircraft · 19
Performance variations in high aspect ratio subsonic diffusers due to geometric constraints in supersonic tactical aircraft inlet installations
1980 · J. SYBERG, J. KONCSEK, et al. · AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit · 10
Bleed system design technology for supersonic inlets
1972 · J. SYBERG, J. KONCSEK · AIAA/SAE Propulsion Joint Specialist Conference · 10
An approach to conformal inlet diffuser design for integrated propulsion systems
1981 · J. KONCSEK · AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit · 6
VSTOL tilt nacelle aerodynamics and its relation to fan blade stresses
1978 · R. SHAW, R. WILLIAMS, et al. · AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit · 5
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Experimental evaluation of a Mach 3.5 axisymmetric inlet
1975 · J. Syberg, J. KONCSEK · NASA STI Repository (National Aeronautics and Space Administration) · 5
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Simulations of a low-boom, axisymmetric, external compression inlet
2013 · T. Coyne, E. Loth, et al. · The Aeronautical Journal · 2
Simulations of a Low-Boom, Axisymmetric, External Compression Inlet
2009 · Terrence Coyne, J Koncsek, et al. · AIAA Fluid Dynamics Conference · 2
Tilt Nacelle Aerodynamics and Its Application to Fan Blade Stresses
1979 · R.J. Shaw, R.C. Williams, et al. · Journal of Aircraft · 2
Extension of CFD technology used to design the JVX inlet
1985 · G. PAYNTER, J. KONCSEK, et al. · AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit · 1
Application of CFD Design Technology in Development of the JVX Engine Inlet
1985 · G.C. Paynter, J.L. Koncsek, et al. · Vertical Flight Society Forum · 1
Operating characteristics of an inlet model tested with a 0.5m powered fan at high angles of attack
1977 · Koncsek, J. L., Shaw, R. J. · NASA STI Repository (National Aeronautics and Space Administration) · 1
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Experimental evaluation of an analytically derived bleed system for a supersonic inlet
1975 · J. SYBERG, J. KONCSEK · AIAA/SAE/ASEE Joint Propulsion Conference (JPC) · 1
HSCT inlet development issues
1992 · J. KONCSEK · NASA Technical Reports Server (NASA)
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Fan inlet for a V/STOL airplane
1977 · J. KONCSEK, J. SYBERG · AIAA/SAE/ASEE Joint Propulsion Conference (JPC)
Works count: 20
Citation count: 134
H-index: 5
I10-index: 4
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