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Friedlander David J.
ID:
1398592
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Friedlander David J.
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Numerical simulations of a Quiet SuperSonic Technology (QueSST) aircraft preliminary design
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Prediction of turbulent diffusing flows using FUN3D
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Understanding the flow physics of shock boundary-layer interactions using CFD and numerical analyses
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Using numerical simulations to explore top-mounted propulsion on a conceptual commercial supersonic transport aircraft
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