Numerical Estimation of Convective Heat Transfer Coefficient and Heat Flux for a Supersonic Rocket Nozzle.
Rocket nozzles are often cooled by passing liquid propellants through channels in the
nozzle walls. Estimating heat transfer to the wall from the hot gases in the nozzle is essential …
nozzle walls. Estimating heat transfer to the wall from the hot gases in the nozzle is essential …
Simulating Wing Thermal Loads at Supersonic Speeds
DJ Cerantola, D Handford, P Dass - AIAA SCITECH 2024 Forum, 2024 - arc.aiaa.org
A sparse parametric conjugate heat transfer CFD analysis using the steady-RANS equations
with the SST turbulence model on a double-wedge airfoil section that factored in altitude …
with the SST turbulence model on a double-wedge airfoil section that factored in altitude …