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Flame temperature, isochoric

The deficiency can be made up, if no energy is added from the outside, only from the detonation products, with a resulting drop in their temperature from the isochoric adiabatic flame temperature. This may quench the chemical reaction. The deficiency diminishes with decrease of wave-front curvature. For point initiation , enough energy must be added from the outside to make up for the total deficit which accumulates during the time the wave is reaching a diameter at which the curvature drops below a critical value... [Pg.267]

Propellant properties pertinent to the problem are density p gas evolution Vg (cm /g), and isochoric flame temperature Ty. From the above, we know the volumes of the vessels Vq and Vi = We also know the masses of the propellants mo and w, = The volume of gas evolved Irom the propellant at standard temperature and pressure (STP) is... [Pg.374]


See other pages where Flame temperature, isochoric is mentioned: [Pg.33]    [Pg.45]    [Pg.428]    [Pg.51]    [Pg.152]    [Pg.2]    [Pg.224]   
See also in sourсe #XX -- [ Pg.151 ]




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