Direct numerical simulation of a supersonic turbulent boundary layer with hydrogen combustion
C Wang, C Xu - Journal of Fluid Mechanics, 2024 - cambridge.org
The complex behaviours of supersonic turbulent boundary-layer flows interacting with
combustion is explored through the use of direct numerical simulations. The chosen flow …
combustion is explored through the use of direct numerical simulations. The chosen flow …
Thermal and drag reduction performance evaluation of a cavity-based scramjet combustor cooled by distributed hydrocarbon film
G Wang, Q Cheng, S Liu, F Li, H Liu - Applied Thermal Engineering, 2025 - Elsevier
Highly robust and efficient cooling methods are crucial to the thermal protection of cavity-
based scramjet combustor. In this work, a novel distributed gas film cooling method using …
based scramjet combustor. In this work, a novel distributed gas film cooling method using …
Investigation of flue gas temperature effects in natural gas fueled Systems: Experimental thermal performance and structural optimization
K Tanriver, M Ay - International Journal of Heat and Fluid Flow, 2024 - Elsevier
This paper presents an innovative approach by employing experimental and analytical
methods to examine the impact of temperature changes in flue gases following combustion …
methods to examine the impact of temperature changes in flue gases following combustion …
Novel exact solutions of momentum and energy equations for hybrid nanofluid flow on a stretching sheet: Whittaker's function-based solutions
A Taghavi, S Dinarvand - Journal of Thermal Analysis and Calorimetry, 2025 - Springer
This study investigates the exact solutions of laminar velocity and thermal boundary layers
of\(\text {Al} _ {2}{\text {O}} _ {3}-\text {CNT}/\text {water}\) hybrid nanofluid flow over a …
of\(\text {Al} _ {2}{\text {O}} _ {3}-\text {CNT}/\text {water}\) hybrid nanofluid flow over a …