| Article ID | Journal | Published Year | Pages | File Type |
|---|---|---|---|---|
| 857085 | Procedia Engineering | 2015 | 7 Pages |
Abstract
Numerical simulation and analysis of aerodynamic characteristics of Soyuz ablation shape is carried out in this paper for the adverse influence coming from recession. The result indicates that the shape change caused by the recession will increase absolute value of trim angle of attack and trim lift-drag ratio. The conclusion offers reference for the aerodynamic layout design and improve of the Soyuz re-entry capsule.
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