scholarly journals Internal Flow Dynamics and Regression Rate in Hybrid Rocket Combustion

2012 ◽  
Vol 13 (4) ◽  
pp. 507-514
Author(s):  
Changjin Lee
AIAA Journal ◽  
1966 ◽  
Vol 4 (4) ◽  
pp. 752-753 ◽  
Author(s):  
EUGENE MILLER

Aerospace ◽  
2019 ◽  
Vol 6 (6) ◽  
pp. 75 ◽  
Author(s):  
Timothy Marquardt ◽  
Joseph Majdalani

In this article, we undertake a concise review of several milestone developments in classical regression rate models of hybrid rocket motors. After a brief description of the physical processes entailed in hybrid rocket combustion, Marxman’s diffusion-limited theory is re-constructed and discussed. Considerations beyond the scope of basic convection-driven models, which address disparate forms of the blowing correction, variable fluid properties, and pressure and radiation effects, are also given. Finally, a selection of kinetically-limited models is presented, with the aim of comparing the characteristics of several competing theories that become applicable under particular circumstances.


2001 ◽  
Vol 17 (1) ◽  
pp. 99-110 ◽  
Author(s):  
Martin J. Chiaverini ◽  
Kenneth K. Kuo ◽  
Arie Peretz ◽  
George C. Harting

Author(s):  
Elizabeth T. Jens ◽  
Victor A. Miller ◽  
Flora S. Mechentel ◽  
Brian J. Cantwell ◽  
Scott Hubbard

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