Research output: Contribution to journal › Article › peer-review
In thin shock layer method is applied to the problem under consideration. A vector of the wing velocity depends on the time. The head shock wave is considered to be joined to the surface of the body at least in an one point. The solution was written for the case when the vertical acceleration component is small.
| Original language | Russian |
|---|---|
| Pages (from-to) | 61-66 |
| Number of pages | 6 |
| Journal | Vestnik Sankt-Peterburgskogo Universiteta. Ser 1. Matematika Mekhanika Astronomiya |
| Issue number | 2 |
| State | Published - 1 Jan 2002 |
ID: 48962810