Numerical Study on Aerodynamic Performance of Mars Parachute Models with Geometric Porosities
The supersonic flows around rigid parachute-like two-body configurations are numerically simulated at Mach number of 1.978 by solving three-dimensional compressible Navier-Stokes equations, where the two-body model consists of a capsule and a canopy, and a geometric structure (i.e., gap) is located...
| Main Authors: | , , , , , , , |
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| Format: | Article |
| Language: | English |
| Published: |
American Association for the Advancement of Science (AAAS)
2022-01-01
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| Series: | Space: Science & Technology |
| Online Access: | http://dx.doi.org/10.34133/2022/9851982 |