NASA NTRS · 19930065828
Turbofan flowfield simulation using Euler equations with body forces
Abstract
A method for flow computations around ducted propfans is presented. The approach is to use the body force terms in the three-dimensional Euler equations to model the propeller. Numerical solutions are compared with experimental data for three ducted propfan configurations for different flow conditions.
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Pankajakshan, Ramesh, Arabshahi, Abdollah, Whitfield, David L.. 1993-06-01. Turbofan flowfield simulation using Euler equations with body forces. https://ntrs.nasa.gov/citations/19930065828
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