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Grumman X-29 CFD Analysis

This page details the CFD analysis of a Grumman X-29 experimental forward-swept jet design. This analysis is an angle of attack sweep from 0-10 degrees at 150 KEAS at 10,000 ft MSL.


The model is a 16.8 million cell poly mesh, analyzed using a segregated solver with an SST K-Omega RANS turbulence model with low Y+.

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