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On the effect of straightening critical and subcritical gas jets. (English) Zbl 0601.76086

The effect of straightening the plane gas jets for Mach numbers \(M\leq 1\) is studied. By means of the asymptotic series of the logarithmic derivative of the Chaplygin function \(x_ v\) corresponding formulae are obtained. These formulae determine the distance at which the jet becomes straight for critical and subcritical velocity on the jet. It is shown that the subsonic jet near critical velocity as well as at critical velocity becomes straight at finite distance from the orifice. The study is done on the model of a gas flowing out an unbounded symmetric container with convergent walls.

MSC:

76N15 Gas dynamics (general theory)
76G25 General aerodynamics and subsonic flows
76M99 Basic methods in fluid mechanics
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