CFD Analysis Process - NASA
-Stretch grid away from wing (15-20%) 7 Glenn Research Center 5) Specify the Boundary Conditions ... determine iterative convergence. • Residuals of conservation equations should approach zero as the number of iterations increases. ... • …
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NASA Hybrid Electric Aircraft Propulsion
www.grc.nasa.govOct 04, 2017 · NASA Hybrid Electric Aircraft Propulsion 1 Dr. Rodger Dyson NIEA Biomimicry Summit Hybrid Gas Electric Propulsion Technical Lead NASA Glenn Research Center Cleveland, OH ... 50 Seat Jet 12 MW Total Propulsive Power 150 Seat 22 MW Total Propulsive Power 1.5-2.6 MW Electric Machines
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