LARGE EDDY SIMULATION OF AN OPTIMIZED HIGHLY-COMPACT SUPERSONIC INLET FEATURING INTERNAL COMPRESSION SPIKES

von Barr, Stephen M.
Veröffentlicht in AIAA SciTech Forum and Exposition (2020 : Orlando, Fla.) High-speed air-breathing propulsion (2020)

EXTENSION OF THE FLAMELET GENERATED MANIFOLD APPROACH TO ACCOUNT FOR HEAT LOSSES IN MULTIPHASE COMBUSTOR SIMULATIONS

von Muralidharan, Balaji
Veröffentlicht in AIAA Propulsion and Energy Forum (2019 : Indianapolis, Ind.) Propellants and combustion (2019)

APPLICATION OF PROGRESS VARIABLE BASED TABULATED CHEMISTRY APPROACH TO INVESTIGATE SPRAY COMBUSTION IN GAS TURBINE ENGINES

von Muralidharan, Balaji
Veröffentlicht in AIAA Propulsion and Energy Forum (2021 : Online) Propellants and combustion (2021)

A MULTI-TIME-SCALE FLAMELET PROGRESS VARIABLE APPROACH IN OPENNCC FOR PREDICTING NOX APPLIED TO COMMERCIAL SUPERSONIC TRANSPORT COMBUSTOR DESIGNS

von Zambon, Andrea C.
Veröffentlicht in AIAA Propulsion and Energy Forum (2020 : Online) Propellants and combustion (2020)