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The use of fractal for prediction of burning rate of composite solid propellants

✍ Scribed by Manouchehr Nikazar; Mohammad B. Bagherpour; Bahram Dabir


Book ID
107431547
Publisher
Springer-Verlag
Year
2000
Tongue
English
Weight
241 KB
Volume
9
Category
Article
ISSN
1003-2169

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πŸ“œ SIMILAR VOLUMES


Dependence of burning rate of composite
✍ R.P. Rastogi; Ram Raj Singh; Anand P. Rao πŸ“‚ Article πŸ“… 1982 πŸ› Elsevier Science 🌐 English βš– 164 KB

Various theories [1,2] have been proposed for the pressure dependence of burning rate of composite propellants since a knowledge of this pressure dependence is vital for the design of a solid propellant rocket motor. Recently, Girdhar and Arora [3] have measured the burning rate of phenol-formaldehy

Erosive burning of composite solid prope
✍ Eugene Miller πŸ“‚ Article πŸ“… 1966 πŸ› Elsevier Science 🌐 English βš– 433 KB

It is assumed thai combustion takes place in the turbulent boundary tay,'~ and that the turbuh,tlt ~lante condsts o/ distorted " [letnwl,'ts" but otheru,ts,, vet,tins on a otob'cular scah' the charact~,ristics o/a laminar l~atne. /| /tat-pb~t,' heat-tran,~/rr ~:orv, latton wah a /actor/or truttspira

Burning Rate Evaluation of Composite Sol
✍ V. Swaminathan; M. Soosaimarian πŸ“‚ Article πŸ“… 1981 πŸ› John Wiley and Sons 🌐 English βš– 403 KB

## Abstract One of the principal parameters associated with a solid propellant is its linear burning rate. Many attempts have been made in the past to determine theoretically the burning rates of solid propellants by the use of appropriate combustion models. The object of the present paper is to pr

Burning rates of solid propellants
✍ J. M. Smith πŸ“‚ Article πŸ“… 1960 πŸ› American Institute of Chemical Engineers 🌐 English βš– 772 KB
Pressure dependence of burning rate of n
✍ H.L. Girdhar; A.J. Arora; G.N. Malik πŸ“‚ Article πŸ“… 1980 πŸ› Elsevier Science 🌐 English βš– 221 KB

Polymers of o-, m-, and p-nitrophenols with formaldehyde were used as fuel binders in composite propellants based on NH 4C]O 4 and KCIO 4 oxidizers. A study of the burning rate in nitrogen has revealed the occurrence of a breakpoint at about 3-5 atm in the burning rate-pressure curves of all six typ