Modeling of response of combustion chamber of high-altitude engine to abnormal power impacts during ground firing tests
S. A. Vladimirov , V. A. Titov , M. A. Kondratenko , D. V. Kornev , S. I. Trefilov , V. D. Gorokhov , S. N. Zherebchikov
Izvestiya MGTU MAMI ›› 2015, Vol. 9 ›› Issue (2-4) : 51 -58.
Modeling of response of combustion chamber of high-altitude engine to abnormal power impacts during ground firing tests
This article proposes a calculation-experimental method of determining the RMS of voltage levels in a sub-camera area of 14D23 high-rise four-chamber engine in terms of ground-based firing tests under the action of abnormal pulsation effects (side forces).
liquid-propellant rocket / side force / linear system / transmission function / correlations / readings of strain gages
Vladimirov S.A., Titov V.A., Kondratenko M.A., Kornev D.V., Trefilov S.I., Gorokhov V.D., Zherebchikov S.N.
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