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A numerical study has been conducted to investigate the unsteady nature of afterbody vortices shed from an upswept region of a simple fuselage configuration. The upsweep angle considered is ϕ=28 d... Click to show full abstract
A numerical study has been conducted to investigate the unsteady nature of afterbody vortices shed from an upswept region of a simple fuselage configuration. The upsweep angle considered is ϕ=28 d...
Keywords:
simulations afterbody;
vortex flows;
high fidelity;
afterbody vortex;
fidelity simulations
Journal Title: AIAA Journal
Year Published: 2019
Link to full text (if available)
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Journal Title: AIAA Journal
Year Published: 2019
Link to full text (if available)
Share on Social Media: Sign Up to like & get
recommendations!