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Since the announcement of a special issue of Shock Waves in honor of Dr. Meng-Sing Liou, the outpouring of manuscripts from his collaborators, colleagues, and friends around the globe has been a fitting tribute to Dr. Liou for his outstanding lifelong achievements and contributions. We received 30 papers in total. The accepted papers are organized into two separate issues. The first issue mainly includes the manuscripts related to the AUSM-family schemes, which was Dr. Liou's crowning work that had the most profound impact. This second issue consists of papers from Meng-Sing's old friends and colleagues, which cover a wide range of topics: numerical methods, gas dynamics, combustion, turbulent flows, hypersonic flows, etc. We are delighted to present these manuscripts as a testimony to Dr. Liou's contributions and accomplishments in these research areas.All 30 submitted papers were subjected to the same rigorous peer review procedure as any regular contribution to Shock Waves. Each paper was reviewed by at least two or more international experts. As a result of peer review, 23 papers were accepted for publication, six papers were rejected, and one was withdrawn by the author. Out of the 23 accepted papers, 14 were accepted after one revision, six papers-after two revisions, and three papers-after three revisions. Ten accepted papers were published in the first issue (volume 29, issue 5), and the remaining 13 papers are included in the present second issue (volume 29, issue 8).Among the contributions of the second issue, we would like to bring our readers' attention to Eleuterio Toro's review paper on the HLLC scheme [1]. The HLLC scheme was originally published in Publisher's Note Springer Nature remains neutral with regard to jurisdictional claims in published maps and institutional affiliations.
Since the announcement of a special issue of Shock Waves in honor of Dr. Meng-Sing Liou, the outpouring of manuscripts from his collaborators, colleagues, and friends around the globe has been a fitting tribute to Dr. Liou for his outstanding lifelong achievements and contributions. We received 30 papers in total. The accepted papers are organized into two separate issues. The first issue mainly includes the manuscripts related to the AUSM-family schemes, which was Dr. Liou's crowning work that had the most profound impact. This second issue consists of papers from Meng-Sing's old friends and colleagues, which cover a wide range of topics: numerical methods, gas dynamics, combustion, turbulent flows, hypersonic flows, etc. We are delighted to present these manuscripts as a testimony to Dr. Liou's contributions and accomplishments in these research areas.All 30 submitted papers were subjected to the same rigorous peer review procedure as any regular contribution to Shock Waves. Each paper was reviewed by at least two or more international experts. As a result of peer review, 23 papers were accepted for publication, six papers were rejected, and one was withdrawn by the author. Out of the 23 accepted papers, 14 were accepted after one revision, six papers-after two revisions, and three papers-after three revisions. Ten accepted papers were published in the first issue (volume 29, issue 5), and the remaining 13 papers are included in the present second issue (volume 29, issue 8).Among the contributions of the second issue, we would like to bring our readers' attention to Eleuterio Toro's review paper on the HLLC scheme [1]. The HLLC scheme was originally published in Publisher's Note Springer Nature remains neutral with regard to jurisdictional claims in published maps and institutional affiliations.
Combustor–turbine interactions are investigated by modeling the unsteady flowfields inside a realistic combustor and high-pressure turbine configuration from the Energy Efficient Engine program. We perform three-dimensional unsteady simulations to capture a liquid-spray fuel/air combustion and relative motions between the combustor and turbine using the Open National Combustion Code. To understand combustor–turbine interactions, we perform both sequential single-component simulations (step 1: [Formula: see text] stator of turbine; step 2: the turbine imposing the time-averaged flow solution from step 1 as the inflow) and a fully coupled combustor–turbine simulation (step 3) at two operating conditions: the simulated sea-level takeoff (SLTO) condition ([Formula: see text]) and a more realistic SLTO ([Formula: see text]). Although the mean flowfields inside the combustor predicted by steps 1 and 3 are similar, there is a noticeable difference in the hot-streak distributions at the first-stage stator. In addition, the shock wave appears at the first-stage stator only for steps 2 and 3 for the low-pressure condition and for step 3 for the high-pressure condition. The calculated turbine efficiencies from step 2 and step 3 differ by about 7%. From both conditions, it is consistently observed that fully coupling the combustor and turbine enhances temporal oscillations of the turbine efficiency through the temperature fluctuations generated in the combustor.
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