| Highly loaded axial flow compressors: history and current developments AJ Wennerstrom | 205 | 1990 |
| Three-dimensional flowfields inside a transonic compressor with swept blades C Hah, AJ Wennerstrom | 122 | 1991 |
| Experimental study of a high-throughflow transonic axial compressor stage AJ Wennerstrom | 96 | 1984 |
| Design of highly loaded axial-flow fans and compressors AJ Wennerstrom (No Title), 2000 | 82 | 2000 |
| Low aspect ratio axial flow compressors: Why and what it means AJ Wennerstrom | 81 | 1989 |
| A three-dimensional model for the prediction of shock losses in compressor blade rows AJ Wennerstrom, SL Puterbaugh | 61 | 1984 |
| Design of a rotor incorporating splitter vanes for a high pressure ratio supersonic axial compressor stage AJ Wennerstrom, GR Frost Aerospace Research Laboratories, Air Force Systems Command, United States …, 1974 | 54 | 1974 |
| Design of a 1500 ft/sec, transonic, high-through-flow, single-stage axial-flow compressor with low hub/tip ratio AJ Wennerstrom, GR Frost Air Force Aero Propulsion Lab Wright-Patterson Afb Oh, 1976 | 45 | 1976 |
| Some experiments with a supersonic axial compressor stage AJ Wennerstrom | 43 | 1987 |
| Investigation of a 1500 ft/sec, transonic, high-through-flow, single-stage axial-flow compressor with low hub/tip ratio AJ Wennerstrom, RD Derose, CW Law, WA Buzzell Aerospace Research Laboratories, Wright-Patterson Air Force Base, AD B 16506, 1976 | 36 | 1976 |
| Test of a supersonic axial compressor stage incorporating splitter vanes in the rotor AJ Wennerstrom, WA Buzzell, RD DeRose Aerospace Research Laboratories, Air Force Systems Command, United States …, 1975 | 35 | 1975 |
| A three-dimensional shock loss model applied to an aft-swept, transonic compressor rotor SL Puterbaugh, WW Copenhaver, C Hah, AJ Wennerstrom | 31 | 1997 |
| A computer program for the specification of axial compressor airfoils GR Frost, RM Hearsey, AJ Wennerstrom Aerospace Research Laboratories, Air Force Systems Command, United States …, 1972 | 30 | 1972 |
| Three-dimensional flowfields inside a transonic compressor with swept blades C Hah, AJ Wennerstrom Turbo Expo: Power for Land, Sea, and Air 79047, V001T01A107, 1990 | 28 | 1990 |
| Vane configuration for fluid wake re-energization AJ Wennerstrom US Patent 4,318,669, 1982 | 27 | 1982 |
| The design of axial compressor airfoils using arbitrary camber lines GR Frost, AJ Wennerstrom Aerospace Research Laboratories, Air Force Systems Command, United States …, 1973 | 26 | 1973 |
| A review of predictive efforts for transport phenomena in axial flow compressors AJ Wennerstrom | 24 | 1991 |
| On the Treatment of body Forces in the radial Equilibrium Equation of Turbomachinery AJ Wennerstrom Traupel commemorative volume.(A 75-19051 06-02) Zurich, Juris-Verlag AG …, 1974 | 21 | 1974 |
| Two axial compressor designs for a stage matching investigation CH Law, AJ Wennerstrom Air Force Wright Aeronautical Laboratories, Wright-Patterson Air Force Base …, 1989 | 20 | 1989 |
| The measurement of turbomachinery stator-to-drum running clearances DP Davidson, RD DeRose, AJ Wennerstrom Turbo Expo: Power for Land, Sea, and Air 79511, V001T01A054, 1983 | 20 | 1983 |
