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Combustion of Composite Propellants

Similar phenomena have also been observed in the combustion of composite propellants. Eisel (El) has observed that there is a unique frequency-pressure relation in a low-pressure region where nonacoustic instability results. He speculates that this preferred frequency is related to the periodic appearance and depletion of the aluminum particles on the propellant surface. High-speed pictures confirm the periodic sluffing of aluminum, but its relation to the preferred frequency is still not clear. [Pg.57]

See other pages where Combustion of Composite Propellants is mentioned: [Pg.1]    [Pg.35]    [Pg.181]    [Pg.182]    [Pg.184]    [Pg.186]    [Pg.188]    [Pg.190]    [Pg.192]    [Pg.194]    [Pg.196]    [Pg.198]    [Pg.200]    [Pg.202]    [Pg.204]    [Pg.206]    [Pg.208]    [Pg.210]    [Pg.214]    [Pg.216]    [Pg.218]    [Pg.220]    [Pg.222]    [Pg.224]    [Pg.226]    [Pg.228]    [Pg.230]    [Pg.232]    [Pg.181]    [Pg.182]    [Pg.184]    [Pg.186]    [Pg.188]    [Pg.190]    [Pg.192]    [Pg.194]    [Pg.196]    [Pg.198]    [Pg.200]    [Pg.202]    [Pg.204]    [Pg.208]    [Pg.210]    [Pg.212]    [Pg.214]    [Pg.216]    [Pg.218]    [Pg.220]    [Pg.222]   


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