| Article ID | Journal | Published Year | Pages | File Type |
|---|---|---|---|---|
| 1718881 | Aerospace Science and Technology | 2008 | 7 Pages |
Abstract
The following paper reports on experimental investigations on high-speed missile control. The paper looks especially at the interference effects of side jets with supersonic cross flow. Detailed wall pressure measurements are presented for three different jet configurations. The shock structure is shown with Schlieren images and the wall streamlines are visualised with oil flow technique.
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Physical Sciences and Engineering
Engineering
Aerospace Engineering
