A review of acoustic dampers applied to combustion chambers in aerospace industry
D Zhao, XY Li - Progress in Aerospace Sciences, 2015 - Elsevier
In engine combustion systems such as rockets, aero-engines and gas turbines, pressure
fluctuations are always present, even during normal operation. One of design prerequisites …
fluctuations are always present, even during normal operation. One of design prerequisites …
An energy management strategy for plug-in hybrid electric vehicles based on deep learning and improved model predictive control
X Sun, J Fu, H Yang, M ** performance of a Helmholtz resonator: Effects of geometry, grazing and bias flow
G Wu, Z Lu, X Xu, W Pan, W Wu, J Li, J Ci - Aerospace Science and …, 2019 - Elsevier
In this work, the effects of the grazing flow and its geometric dimensions on the
aeroacoustics dam** performance of a Helmholtz resonator are numerically evaluated …
aeroacoustics dam** performance of a Helmholtz resonator are numerically evaluated …
Control of combustion instability with a tunable Helmholtz resonator
Z Zhang, D Zhao, N Han, S Wang, J Li - Aerospace Science and …, 2015 - Elsevier
Unwanted combustion instability occurs in many propulsion systems, such as rocket motors,
and aero-engines. It is typically caused by a coupling between acoustic waves and unsteady …
and aero-engines. It is typically caused by a coupling between acoustic waves and unsteady …