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Visualization of flowfield surrounding a Crew Launch Vehicle concept

High-Fidelity Simulations Supporting Crew Abort Risk

Flowfield surrounding a Crew Launch Vehicle concept computed using OVERFLOW-2, showing Mach contours in a plane of symmetry for supersonic flow.

Credit: Research by Scott Lawrence, Donnovan Mathias, Jerry Yan, Goetz Klopfer, Jeff Onufer, Shishir Pandya, Mike Olsen, William Chan, NASA Ames Research Center.

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