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Effect of Operating Conditions and Design on Afterburner PerformanceAfterburners for turbojet engines have, within the past decade, found increasing application in service aircraft. Practically all engines manufactured today are equipped with some form of afterburner, and its use has increased from what was originally a short-period thrust-augmentation application to an essential feature of the turbojet propulsion system for flight at supersonic speeds. The design of these afterburners has been based on extensive research and development effort in expanded laboratory facilities by both the NACA and the American engine industry. Most of the work of the engine industry, however, has either not been published or is not generally available owing to its proprietary nature. Consequently, the main bulk of research information available for summary and discussion is of NACA origin. However, because industrial afterburner development has closely followed NACA research, the omission is more one of technical detail than method or concept. One principal difficulty encountered in summarizing the work in this field is that sufficient knowledge does not yet exist to rationally or directly integrate the available background of basic combustion principles into combustor design. A further difficulty is that most of the experimental investigations that have been conducted were directed chiefly toward the development of specific afterburners for various engines rather than to the accumulation of systematic data. This work has, nonetheless, provided not only substantial improvements in the performance of afterburners but also a large fund of experimental data and an extensive background of experience in the field. Consequently, it is the purpose of the present chapter to summarize the many, and frequently unrelated, experimental investigations that have been conducted rather than to formulate a set of design rules. In the treatment of this material an effort has been made, however, to convey to the reader the "know how" acquired by research engineers in the course of afterburner studies.
Document ID
19670095388
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Fleming, W. A.
(NASA Lewis Research Center Cleveland, OH, United States)
Gabriel, D. S.
(NASA Lewis Research Center Cleveland, OH, United States)
Lundin, B. T.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
August 3, 2013
Publication Date
May 2, 1956
Publication Information
Publication: Adaptation of Combustion Principles to Aircraft Propulsion. Volume II - Combustion in Air-Breathing Jet Engines
Subject Category
Aircraft Propulsion And Power
Accession Number
67X87775
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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