Abstract
Using detailed investigations of anisentropic supersonic wave patterns in cascades of flat plates it is shown that four sharply distinguishable types of flow are possible in these flow configurations. The existence of these types is proved and possibilities of transition from one type to the other are mentioned. To determine the characteristic diagram of a given cascade configuration the Herzkurven method is employed for the computation of anisentropic supersonic flow regions and the fundamental equations of gas dynamics. Some numerical results are disclosed.
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