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Eight-channel frequency-response test of the cylindrical-shell-and-ring assembly in the range 1000 to 8000 Hz
Authors: Arinchev S.V. | Published: 18.10.2022 |
Published in issue: #11(752)/2022 | |
Category: Aviation, Rocket and Technology | Chapter: Aircraft Strength and Thermal Modes | |
Keywords: detonation jet propulsion, Auger effect, Fourier hypothesis |