On supersonic flow behind a curved shock
نویسندگان
چکیده
منابع مشابه
Determination of Shock Standoff Distance for Wedge at Supersonic Flow
An experimental investigation is conducted to calculate the shock standoff (SSO) distance in front of an acute-angled wedge. For this experimentation, simple water flows channel analysis is carried out. The flow velocity is varied from 13.2 cm/s to 25.5 cm/s increasing in steps of 1 cm/s. A velocity of 13.2 cm/s corresponds to Froude number 1.13 and velocity of 25.5 cm/s to Froude number 1.41. ...
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ژورنال
عنوان ژورنال: Quarterly of Applied Mathematics
سال: 1957
ISSN: 0033-569X,1552-4485
DOI: 10.1090/qam/83327