Propellants and combustion / American Institute of Aeronautics and Astronautics ; Volume 1 of 2
Propellants and combustion / American Institute of Aeronautics and Astronautics ; Volume 2 of 2
NUMERICAL STUDY ON COMBUSTION CHARACTERISTIC OF MICRON ALUMINUM PARTICLE
CHARACTERIZATION OF THE MELT LAYER OF AMMONIUM PERCHLORATE SINGLE
TOWARDS A SIMULATION METHOD FOR ALUMINUM-PARTICLE-ENHANCED SOLID FUEL COMBUSTION DEVICES
LASER INDUCED SPARK IGNITION OF LAMINAR PREMIXED METHANE AIR JETS
DETERMINATION OF NITRIC OXIDE CONCENTRATIONS IN MIXTURES WITH NITROGEN TETROXIDE VIA IR SPECTROMETRY
INVESTIGATION OF COMBUSTION INSTABILITIES IN A FULL FLOW STAGED COMBUSTION MODEL ROCKET COMBUSTOR
STUDIES ON FLAME SPREAD ACCELERATION, DETONATION KERNEL IN A DUAL-THRUST ROCKET
PILOT INJECTOR REDESIGN TO REDUCE N+3 CYCLE EMISSIONS FOR A GAS-TURBINE COMBUSTOR
EVALUATION OF PLATEAU BURNING BEHAVIOR IN HTPB-AP-AL COMPOSITE PROPELLANTS
FLOW FIELD CHARACTERIZATION OF A THIRD GENERATION SWIRL-VENTURI LEAN DIRECT INJECTOR
NUMERICAL STUDY OF NONLINEAR SELF-SUSTAINED THERMOACOUSTIC INSTABILITY IN A SWIRLING COMBUSTOR
TURBULENT NONPREMIXED JET FLAMES UNDER TRANSVERSE ACOUSTIC FORCING
BREAKUP CHARACTERISTICS AND FAR-FIELD TRAJECTORY OF LIQUID JETS IN SUBSONIC CROSSFLOW
EXPERIMENTAL AND NUMERICAL STUDY OF METHANE-OXYGEN COMBUSTION INSIDE A LOW PRESSURE ROCKET MOTOR
PERFORMANCE COMPARISON OF DATA-DRIVEN REDUCED MODELS FOR A SINGLEINJECTOR COMBUSTION PROCESS