Analysis of self-excited transverse combustion instability in a rectangular model rocket combustor
K Guo, Y Ren, Y Tong, W Lin, W Nie - Physics of Fluids, 2022 - pubs.aip.org
A methane/oxygen mixture is considered to be an appropriate propellant for many future
rocket engines due to its practicality and low cost. To better understand the combustion …
rocket engines due to its practicality and low cost. To better understand the combustion …
Combustion response of shear coaxial injectors to transverse combustion instabilities
Transverse combustion instabilities observed in a multi-element oxidizer-rich staged
combustion (ORSC) cycle based model rocket combustor operating at 1.15 MPa are …
combustion (ORSC) cycle based model rocket combustor operating at 1.15 MPa are …
Three-Dimensional Numerical Analysis of Longitudinal Thermoacoustic Instability in a Single-Element Rocket Combustor
G Kangkang, X Boqi, R Yongjie, T Yiheng… - Frontiers in Energy …, 2022 - frontiersin.org
This study numerically investigated the thermoacoustic combustion instability characteristics
of a scaled rocket combustor based on a hybrid of the Reynolds-averaged Navier–Stokes …
of a scaled rocket combustor based on a hybrid of the Reynolds-averaged Navier–Stokes …
Experimental Investigation of Stochastically Forced Rijke-Type Supercritical Thermoacoustic Systems
Intense thermoacoustic oscillations may lead to severe deterioration due to the induced
intolerable damage to combustors. A better understanding of unstable behaviors is …
intolerable damage to combustors. A better understanding of unstable behaviors is …