Gerald C. Paynter

发表

NUMERICAL MODELING OF THREE-DIMENSIONAL FLOWS IN TURBOFAN ENGINE EXHAUST NOZZLES

Stanley F. Birch, D. B. Spalding, D. G. Tatchell, 1978 .

Comparison of Full Potential and Euler Solution Algorithms for Aeropropulsive Flowfield Computations

S.N.B. Murthy, Gerald C. Paynter, 1986 .

Modeling the Response from a Cascade to an Upstream Acoustic Disturbance

Gary L. Cole, Gerald C. Paynter, Larry T. Clark, 2000 .

Numerical Methods for Engine-Airframe Integration

S.N.B. Murthy, Gerald C. Paynter, 1986 .

Evaluating the temporal accuracy of inlet normal shock propagation simulations

Gerald C. Paynter, David W. Mayer, 1995 .

“Fuel Flow Method2” for Estimating Aircraft Emissions

Douglas P. DuBois, Gerald C. Paynter, G. Paynter, 2006 .

Prediction of supersonic inlet unstart caused by freestream disturbances

Gerald C. Paynter, David W. Mayer, 1994 .

Response of a two-dimensional cascade to an upstream disturbance

Gerald C. Paynter, G. Paynter, 1997 .

Implementation of a Compressor Face Boundary Condition Based on Small Disturbances

John W. Slater, Gerald C. Paynter, J. Slater, 2000 .

Flow stability issues in supersonic inlet flow analyses

Gerald C. Paynter, E. Tjønneland, G. Paynter, 1993 .