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Gerald C. Paynter

Observed names: G. C. Paynter, G. PAYNTER, G. Paynter, G.C. Paynter, GERALD C. PAYNTER, GERALD PAYNTER, Gerald Paynter, Paynter, G. C., Paynter, Gerald C., author.
Observed institution: Boeing (United States)
OpenAlex ID: A5088043035
“Fuel Flow Method2” for Estimating Aircraft Emissions
2006 · Doug DuBois, Gerald C. Paynter · SAE technical papers on CD-ROM/SAE technical paper series · 163
Prediction of supersonic inlet unstart caused by freestream disturbances
1995 · David W. Mayer, Gerald C. Paynter · AIAA Journal · 97
Boundary conditions for unsteady supersonic inlet analyses
1994 · David W. Mayer, Gerald C. Paynter · AIAA Journal · 88
Use of Coles' universal wake function for compressible turbulent boundary layers
1970 · DOUGLAS C. MATHEWS, MORRIS E. CHILDAS, et al. · Journal of Aircraft · 46
Modeling supersonic inlet boundary-layer bleed roughness
1993 · Gerald C. Paynter, David A. Treiber, et al. · Journal of Propulsion and Power · 28
Numerical Modeling of Three-Dimensional Flows in Turbofan Engine Exhaust Nozzles
1978 · Stanley F. Birch, Gerald C. Paynter, et al. · Journal of Aircraft · 27
Nozzle Exit Flow Profile Shaping for Jet Noise Reduction
1977 · R. W. Crouch, C. L. Coughlin, et al. · Journal of Aircraft · 26
An experimental and numerical study of the 3-D mixing flows of a turbofan engine exhaust system
1977 · S. BIRCH, G. PAYNTER, et al. · 15th Aerospace Sciences Meeting · 18
Modeling the Response from a Cascade to an Upstream Acoustic Disturbance
2000 · Gerald C. Paynter, Larry T. Clark, et al. · AIAA Journal · 17
Lag model for turbulent boundary layers over rough bleed surfaces
1994 · J. Lee, M. L. Sloan, et al. · Journal of Propulsion and Power · 17
Modified Spalart-Allmaras one-equation turbulence model for rough wall boundary layers
1996 · Jaesoo Lee, Gerald C. Paynter · Journal of Propulsion and Power · 16
Response of a Two-Dimensional Cascade
1997 · Gerald C. Paynter · AIAA Journal · 14
Flow stability issues in supersonic inlet flow analyses
1993 · GERALD PAYNTER, DAVID MAYER, et al. · AIAA Aerospace Sciences Meeting · 14
Shock-wave reflection from a turbulent boundary layer with mass bleed.
1968 · WILLIAM R. SEEBAUGH, GERALD C. PAYNTER, et al. · Journal of Aircraft · 14
Hybrid Turbulence Models for Unsteady Simulation of Jet Flows
2002 · Mortaza Mani, Gerald Paynter · AIAA Fluid Dynamics Conference and Exhibit · 13
Response of a two-dimensional cascade to an upstream disturbance
1997 · Gerald C. Paynter · AIAA Journal · 12
Prediction of supersonic inlet unstart caused by freestream disturbances
1994 · David Mayer, Gerald Paynter · 32nd Aerospace Sciences Meeting and Exhibit · 11
Nozzle exit flow profile shaping for jet noise reduction
1976 · R. CROUCH, C. COUGHLIN, et al. · Aeroacoustics Conference · 11
Implementation of a Compressor Face Boundary Condition Based on Small Disturbances
2000 · John W. Slater, Gerald C. Paynter · Volume 1: Aircraft Engine; Marine; Turbomachinery; Microturbines and Small Turbomachinery · 8
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Modeling the response from a cascade to an upstream convective velocity disturbance
1998 · Gerald Paynter · AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit · 7
A lag model for turbulent boundary layers developing over rough bleed surfaces
1993 · J. LEE, M. SLOAN, et al. · AIAA Fluid Dynamics, Plasma Dynamics and Lasers Conference · 7
Modeling supersonic inlet boundary layer bleed roughness
1992 · GERALD PAYNTER, DAVID TREIBER, et al. · AIAA Aerospace Sciences Meeting and Exhibit · 7
Analysis of Weak Glancing Shock/Boundary-Layer Interactions
1980 · G.C. Paynter · Journal of Aircraft · 7
Progress toward the analysis of supersonic inlet flows
1983 · G. PAYNTER, H. CHEN · AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit · 6
Implementation of a Compressor Face Boundary Condition Based on Small Disturbances
2000 · John W. Slater, Gerald C. Paynter · Journal of Turbomachinery · 5
Works count: 58
Citation count: 721
H-index: 14
I10-index: 18
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