OPERATIONAL CHARACTERISTICS OF A ROCKET-TYPE RDE USING C2H4/GO2

von Han, Hyung-Seok
Veröffentlicht in AIAA Propulsion and Energy Forum (2019 : Indianapolis, Ind.) Pressure gain combustion (2019)

DESIGN OF SHAPE TRANSITION NOZZLE FOR DIRECT-CONNECT SUPERSONIC COMBUSTOR

von Sung, Bu-Kyeng
Veröffentlicht in AIAA Propulsion and Energy Forum (2021 : Online) High-speed air-breathing propulsion (2021)

DYNAMIC MODE DECOMPOSITION (DMD) ANALYSIS OF THE DETONATION CELLBIFURCATION PROCESS

von Pavalavanni, Pradeep K.
Veröffentlicht in AIAA Propulsion and Energy Forum (2021 : Online) Pressure gain combustion (2021)

COMPUTATIONAL ANALYSIS OF INTERNAL FLOW AND THERMAL ENVIRONMENT IN A SCRAMIJET ENGINE BEFORE IGNITION

von Kim, Jae-Eun
Veröffentlicht in AIAA Propulsion and Energy Forum (2021 : Online) High-speed air-breathing propulsion (2021)

COMPARISON OF UPPER-STAGE ENGINE OPTIONS FOR SMALL LAUNCH VEHICLE BASED ON KSLV-II

von Jo, Min-Seon
Veröffentlicht in AIAA Propulsion and Energy Forum (2021 : Online) Liquid propulsion (2021)

COMPARISON OF HYDROGEN COMBUSTION MECHANISMS FOR UNSTEADY SHOCKINDUCED COMBUSTION WITH DYNAMIC MODE DECOMPOSITION (DMD) ANALYSIS

von Pavalavanni, Pradeep K.
Veröffentlicht in AIAA Propulsion and Energy Forum (2021 : Online) Pressure gain combustion (2021)

INJECTOR DESIGN II TWO-PHASE FLOW STUDY OF THE RD-0110 ENGINE INJECTOR WITH DIFFERENT RECESS LENGTHS

von Natarajan, Vishnu
Veröffentlicht in AIAA Propulsion and Energy Forum (2021 : Online) Liquid propulsion (2021)

Analysis on Flow-Field Characteristics of a Scramjet Combustor with Respect to Equivalence Ratio Using IDDES Simulation

von Jeong, Seung-Min
Veröffentlicht in AIAA SciTech Forum (2023 : National Harbor, Md.; Online) High-speed air-breathing propulsion (2023)

NUMERICAL SIMULATION OF COMBUSTION INSTABILITY IN A DIRECT-CONNECT SUPERSONIC COMBUSTOR

von Jeong, Seung-Min
Veröffentlicht in AIAA Propulsion and Energy Forum (2021 : Online) High-speed air-breathing propulsion (2021)

OPERATING CHARACTERISTICS OF NON-CIRCULAR TRI-ARC ROTATING DETONATION ENGINE (RDE)

von Lee, Eun Sung
Veröffentlicht in AIAA Propulsion and Energy Forum (2021 : Online) Pressure gain combustion (2021)

NUMERICAL SIMULATION OF A GH2/LOX ROCKET COMBUSTOR WITH MULTIPLE INJECTORS USING REAL GAS FLAMELET MODEL

von Hwang, Won-Sub
Veröffentlicht in AIAA Propulsion and Energy Forum (2019 : Indianapolis, Ind.) Propellants and combustion (2019)