Яндекс.Метрика

 S.G. Kundasev, N.P. Kiselev, V.I. Zapryagaev

Issue: 1 , Volume: 1770 , Уear of publication: 2016
Serial edition: AIP Conference Proceedings. 18th International Conference on the Methods of Aerophysical Research (ICMAR2016) (Perm, Russia, 27 June-3 July, 2016)
Pages: 030031-1-030031-10

Abstract

Experimental data gained while studying the gas-dynamic structure of a supersonic jet impinging onto a flat plate are reported. The data, obtained for different obstacle inclination angles and flow regimes, comprise the near-wall pressure fields and schlieren images of the flow. The flow pattern in the vicinity of the obstacle and the main elements of the shock-wave structure of the flow observed at various inclination angles are described.
индекс в базе ИАЦ: 047692