Effects of local flow field on chemical reactions in thin reaction zone of premixed flames

Author(s):  
T. Takeno ◽  
M. Nishioka ◽  
X. L. Zhu ◽  
H. Yamashita
2017 ◽  
Vol 100 (1) ◽  
pp. 177-196 ◽  
Author(s):  
Christopher Jainski ◽  
Martin Rißmann ◽  
Suad Jakirlic ◽  
Benjamin Böhm ◽  
Andreas Dreizler

Author(s):  
Chiara Palomba

Rotating stall is an instability phenomenon that arises in axial flow compressors when the flow is reduced at constant rotational speed. It is characterised by the onset of rotating perturbations in the flow field accompanied by either an abrupt or gradual decrease of performances. Although the flow field is unsteady and non axisymmetric, the global operating point is stable and a stalled branch of performance curve may be experimentally determined. The number, rotational speed, circumferential extension of the rotating perturbed flow regions named rotating cells may vary from one compressor to another and may depend on the throttle position. The present work focuses on the interaction between local flow parameters and global compressor performance parameters with the aim of reaching a better understanding of the phenomenon. Starting from the Day, Greitzer and Cumpsty [1] model the detailed flow conditions during rotating stall are studied and related to the global performance parameters. This is done both to verify if the compressor under examination fits to the model and if the detailed flow structure may highlight the physics that in the simple model may hide behind the correlation’s used.


The fundamental physical, chemical and mechanical processes which occur when a detonation wave passes through an explosive were imperfectly understood at the beginning of the recent war. As part of the scientific war effort in the British Common-wealth and in the United States of America, many theoretical and experimental studies were made of detonation processes. Much of the work has recently been declassified and some has been published. Several centres of research in this country and elsewhere are vigorously continuing with these studies. As later papers will show, the quality and general scientific interest of much of this work was considered sufficient to form the basis of a Discussion of the Royal Society. If one neglects the finite width of the zone in the detonation front where chemical reactions occur, a freely running steady plane detonation front can only advance through an explosive with the Chapman-Jouguet velocity defined by D = u + c . Once the explosive products are formed, their subsequent chemical reactions and motion in the detonation front may be considered as adiabatic. Although Chapman (1899) and Jouguet (1901) correctly stated their equation, neither attempted to discuss the reaction zone itself. It was therefore thought necessary that the recent views on the reaction zone should be described in a manner which throws new light on the Chapman-Jouguet equation. Professor J. von Neumann, Dr⋅ S. F. Boys and Dr A. F. Devonshire were the principal contributors on the theoretical side and von Neumann’s theory (1942) will be outlined later.


2016 ◽  
Vol 116 (13) ◽  
Author(s):  
David Schäffel ◽  
Kaloian Koynov ◽  
Doris Vollmer ◽  
Hans-Jürgen Butt ◽  
Clarissa Schönecker

2011 ◽  
Vol 47 (6) ◽  
pp. 679-690 ◽  
Author(s):  
Gašper Benedik ◽  
Brane Širok ◽  
Igor Markič ◽  
Matjaž Eberlinc

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