Combustion dynamics characteristics and fuel pressure modulation responses of a three-cup third-generation swirl-venturi lean direct injection combustion concept /

Bibliographic Details

Main Author:	He, Zhuohui J. (Author)
Format:	Government Document eBook
Language:	English
Published:	Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, April 2020.
Series:	NASA technical memorandum ; 2020-220522.
Subjects:	Fuel injection. Combustion. Combustion chambers. Noise measurement. Fuel-air ratio.
Online Access:	https://purl.fdlp.gov/GPO/gpo137464