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MAXIMUM PRINCIPLE FOR SUBSONIC FLOW WITH VARIABLE ENTROPY

2017
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Naučnyj Vestnik MGTU GA
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Maximum principle for subsonic flow is fair for stationary irrotational subsonic gas flows. According to this principle, if the value of the velocity is not constant everywhere, then its maximum is achieved on the boundary and only on the boundary of the considered domain. This property is used when designing form of an aircraft with a maximum critical value of the Mach number: it is believed that if the local Mach number is less than unit in the incoming flow and on the body surface, then the

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