An Approximate Distribution of Particle Mass Flux in a High Altitude Solid Propellant Rocket Plume
Author:
Affiliation:
1. The Aerospace Corporation, El Segundo, Calif.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.49328
Reference5 articles.
1. Analytical approximation for the flow from a nozzle into a vacuum.
2. a) Select coordinates g!,<„ governing the internal configuration of 5 in such a way that q^ = • •- = qn= 0 during the simple spin to be investigated, and form V and Dr(r = 1, ri) such that the requirements imposed by Eqs. (2-4) of Ref. 1 are satisfied.
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1. Multiburst cloud rise - Theory and experiment;Journal of Thermophysics and Heat Transfer;1988-10
2. Simple model for particle radiative transfer in vacuum particle plumes;Journal of Thermophysics and Heat Transfer;1988-10
3. REFERENCES;Fundamentals of Gas Particle Flow;1980
4. Analytical model for a two-phase vacuum plume;AIAA Journal;1976-02
5. High temperature reformation of aluminum and chlorine compounds behind the Mach disk of a solid-fuel rocket exhaust;Atmospheric Environment (1967);1976-01
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