burning rate - Globe Thesis

Keyword [burning rate] Result: 41 - 60 \| Page: 3 of 4
41.	Research On Key Technologies Of Lightweight 82mm Recoilless Gun
42.	Synthesis And Catalytic Performance Of Binuciear Ferrocenyl Compounds And Metal Complexes
43.	Multidimensional modeling of solid propellant burning rates and aluminum agglomeration and one-dimensional modeling of RDX/GAP and AP/HTPB
44.	Flame surface density of turbulent premixed flames at medium to high turbulence intensities
45.	Effects of crossflow on burning rates of rectangular methanol pool fires
46.	Monte Carlo assessment of solid propellant burning rate measurement
47.	Numerical simulation of an open premixed turbulent V-flame using contour advection with surgery: Determination of flame surface density and overall burning rate
48.	Experimental investigation of liquid and gas fueled flames towards the development of a burning rate emulator (BRE) for microgravity applications
49.	Measurement apparatus and modelling of laminar burning speed and mass burning rate of syngas and onset of auto-ignition of n-heptane and gas to liquid fuel
50.	Inclusion of nanostructured materials in composite and double base propellant
51.	Modeling the steady-state combustion of solid propellant ingredients with detailed kinetics
52.	Ultrasonic technique resolution for solid propellant burning rate measurement
53.	Ballistic characteristics of bi-plateau solid propellants
54.	The effect of radiative heat feedback on burning rate of metalized propellants
55.	COMBUSTION CHARACTERISTICS OF SOLVENT REFINED COAL AS A SOLID ROCKET FUEL
56.	Experimental And Numerical Investigations On Combustion And Agglomeration Characteristics Of Solid-Fuel Ramjet
57.	Research On Algorithms For Dynamic Nonuniform Regression Of Solid Rocket Motors And Its Application
58.	Study On The Rotating Flow And Combustion Characteristics Of Multi-pool Fire Whirl In Side Slit Vertical Channel
59.	Research On Ultrasonic Measurement Method Of Burning Rate Of Solid Propellant In Motor
60.	Numerical Simulation Research On Unsteady Flow Field In Launching Chamber
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