Research output: Contribution to journal › Article › peer-review
The 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 as joined to the front edge of the wing. The solution is written in the finite form.
| Original language | Russian |
|---|---|
| Pages (from-to) | 69-73 |
| Number of pages | 5 |
| Journal | Vestnik Sankt-Peterburgskogo Universiteta. Ser 1. Matematika Mekhanika Astronomiya |
| Issue number | 3 |
| State | Published - 1 Jan 2002 |
ID: 48962881