Increasing the frontal thrust of a pulsating thermojet with a constant-volume multicavity combustion chamber |
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| Authors: | V. I. Bogdanov A. K. Dormidontov K. S. P’yankov M. N. Toporkov |
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| Affiliation: | 1. Solov??ev Rybinsk State Aviation-Technology University, Rybinsk, Russia
2. Baranov Central Institute of Aviation Materials, Moscow, Russia
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| Abstract: | The operation of a pulsating thermojet with a constant-volume multicavity combustion chamber is studied by means of a mathematical model. The engine??s thrust ensures supersonic flight. |
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