NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Press Enter or click the Search button to begin your search.

Back to Results
Stretched Diffusion Flames in von Karman Swirling FlowsFlame stretch plays a critical role in determining the fundamental characteristics of a diffusion flame, including its extinction and burning efficiencies. The concept of 'flame stretch' to characterize the effects of straining flows on flames was first introduced by Karlovitz (1953). Following his work, this concept was further exploited to characterize flame dynamics by a number of authors including Lewis and von Elbe (1961), and Markstein (1964). The mathematical definition of flame stretch and its physical meanings can be found in the review article by Law (1988). Most of the experimental studies on stretched diffusion flames thus far have been in the high velocity, high stretch regime. Under normal gravity conditions high temperature differences encountered in a flame causes buoyancy induced flows making it difficult to obtain low flow, low stretch flames in practice. Even the experiments in the high-stretch regime employ flow configurations that are essentially two-dimensional. The three dimensionality of the swirling flow field observed in many common combustion devices are missing in these configurations. The most commonly used experimental configurations are the counter flow diffusion flames, stagnation-point boundary layers, spherically symmetric combustion such as droplet combustion or porous sphere combustion with injected fuel, cylindrical flames and flat flame burners. The nature of the influences of the swirl on the structure and extinction of diffusion flames have not been addressed in any great detail thus far in the literature.
Document ID
19970020590
Acquisition Source
Glenn Research Center
Document Type
Conference Paper
Authors
Vedha Nayagam
(Analex Corporation Brook Park, OH United States)
Forman A Williams
(University of California San Diego San Diego, United States)
Date Acquired
August 17, 2013
Publication Date
May 1, 1997
Publication Information
Publication: Fourth International Microgravity Combustion Workshop
Publisher: National Aeronautics and Space Administration
Subject Category
Inorganic, Organic and Physical Chemistry
Report/Patent Number
NASA-CP-10194
Meeting Information
Meeting: Fourth International Microgravity Combustion Workshop
Location: Cleveland, OH
Country: US
Start Date: May 19, 1997
End Date: May 21, 1997
Sponsors: National Aeronautics and Space Administration
Accession Number
97N21863
Distribution Limits
Public
Copyright
Portions of document may include copyright protected material.
Technical Review
NASA Technical Management
Document Inquiry

Available Downloads

There are no available downloads for this record.
No Preview Available