top of page

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+.

Fields_X-29_Project2_Converged_A_6.0__0312_Corrected_PolyAircraftMesh.png

Fields_X-29_Project2_Converged_A_6.0__0312_Corrected_Refinements.png

Fields_X-29_Project2_Converged_A_6.0__0312_Corrected_Y+ (1).png

Fields_X-29_Project2_Converged_A_6.0__0312_Corrected_SurfaceMeshOriginal.png

Fields_X-29_Project2_Converged_A_6.0__0312_Corrected_VectorShearStress and Pressure RV4.pn

Fields_X-29_Project2_Converged_A_6.0__0312_Corrected_Total Pressure and Vorticity RV2.png

Fields_X-29_Project2_Converged_A_10.0_Corrected_ReversedFlow.png

Fields_X-29_Project2_Converged_A_6.0__0312_Corrected_Total Pressure and Pressure RV4.png

Fields_X-29_Project2_Converged_A_6.0__0312_Corrected_Residuals (1).png

Fields_X-29_Project2_Converged_A_6.0__0312_Corrected_PolyFarField.png

bottom of page