Propellants and combustion / American Institute of Aeronautics and Astronautics ; Volume 2 of 2
Propellants and combustion / American Institute of Aeronautics and Astronautics ; Volume 1 of 2
NUMERICAL STUDY ON COMBUSTION CHARACTERISTIC OF MICRON ALUMINUM PARTICLE
FLAME SPEED OF TURBULENT PREMIXED KERNEL IN TURBULENT FLOWS
FLOW FIELD CHARACTERIZATION OF A THIRD GENERATION SWIRL-VENTURI LEAN DIRECT INJECTOR
DEVELOPMENT AND TESTING OF PULSE GUNS FOR COMBUSTION INSTABILITY TESTING
BROADBAND, MID-INFRARED LASER-ABSORPTION MEASUREMENTS OF TEMPERATURE, CH4, AND C3H8 IN FLAMES
UNCERTAINTY QUANTIFICATION ANALYSIS OF RANS OF SPRAY JETS
CHARACTERIZATION OF THE MELT LAYER OF AMMONIUM PERCHLORATE SINGLE
EFFECT OF FUEL TEMPERATURE ON EMISSIONS AND STRUCTURE OF A SWIRLSTABILIZED FLAME
DESIGN AND CHARACTERIZATION OF THE DUAL INDEPENDENT SWIRL COMBUSTOR FACILITY (DISCO)
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
IGNITION OF JET FUEL ASSISTED BY A HOT SURFACE AT AIRCRAFT COMPRESSION IGNITION ENGINE CONDITIONS
HIGH-SPEED VIDEO ANALYSIS OF LUBRICATING OILS UNDERGOING HOT-SURFACE IGNITION
MEASUREMENTS OF THE VAPOR PRESSURE OF LIQUID HYDRAZINE ABOVE ITS NORMAL BOILING POINT
DETERMINATION OF NITRIC OXIDE CONCENTRATIONS IN MIXTURES WITH NITROGEN TETROXIDE VIA IR SPECTROMETRY