Publication Date:
2019-07-13
Description:
This paper overviews the current program, whose objective is to establish the generic technology base for advanced aircraft I.C. engines of the early 1990's and beyond. The major emphasis of this paper is on development of the past two years. Past studies and ongoing confirmatory experimental efforts are reviewed, which show unexpectly high potential when modern aerospace technologies are applied to inherently compact and balanced I.C. engine configurations. Currently, the program is focussed on two engine concepts the stratified-charge, multi-fuel rotary, and the lightweight two-stroke diesel. A review is given of contracted and planned high performance one-rotor and one-cylinder test engine work addressing several levels of technology. Also reviewed are basic supporting efforts, e.g., the development and experimental validation of computerized airflow and combustion process models, being performed in-house at Lewis Research Center and by university grants.
Keywords:
AIRCRAFT PROPULSION AND POWER
Type:
NASA-TM-83668
,
E-2111
,
NAS 1.15:83668
,
Joint Propulsion Conf.; Jun 11, 1984 - Jun 13, 1984; Cincinnati, OH; United States
Format:
application/pdf
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