By V. Yang, M. Habiballah, M. Popp, J. Hulka
This is often the 1st significant e-book on liquid-rocket combustion units because 1960. a complete of 26 chapters ready via world-renowned specialists of their topic parts are integrated. each one bankruptcy makes a speciality of a particular point of liquid-propellant combustion and thrust chamber dynamics, and is integrated into the amount in a well-organized, cohesive demeanour. There are contributions from 9 assorted nations - China, France, Germany, Italy, Japan, The Netherlands, Russia, Sweden, and the U.S..
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Additional info for Liquid Rocket Thrust Chambers (Progress in Astronautics and Aeronautics)
The quantities of fuel pairs and oxidizer pairs need not be equal. A functional advantage can be gained by designing more impinging pairs of the less volatile propellant. Quadlet elements are like-doublet pairs that have been canted toward each other to induce improved unlike propellant mixing. For the same number of impinging pairs and comparable atomization and vaporization efﬁciencies as like-on-like doublets, quadlet injectors tend to deliver higher performance in mixing limited injectors. Unlike doublets impinge a single fuel jet upon a single oxidizer jet.
Impinging Jet Injectors Many variations on the impinging jet injectors shown in Fig. 3 are used for liquid rocket combustion devices. Some major classiﬁcations are like-on-like doublets, quadlet elements, unlike doublets, and unlike triplets. The like-on-like doublet was one of the earliest injection element concepts used for liquid rocket injectors. Its popularity was generally attributable to its stable combustion characteristics while delivering moderate performance. The like-on-like doublet is composed of both self-impinging fuel doublets and selfimpinging oxidizer doublets.
These methods have not found practical applications in commercial LREs. 7) Combined atomization methods using several different kinds of energy. Different conversion techniques can be used simultaneously to intensify atomization, such as combined utilization of the potential energy of liquid and kinetic energy of atomizing gas. Application of vibrational energy during pneumatic and hydraulic atomization produces the most signiﬁcant effect. This combination allows considerable savings of the energy spent for atomization.