Fuel flexible combustor for high-OPR compact-core N+3 propulsion engine : final technical report /

Bibliographic Details

Main Author:	Smith, Lance L. (Author)
Format:	Government Document eBook
Language:	English
Published:	Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, March 2020.
Series:	NASA contractor report ; 2020-220489.
Subjects:	Bypass ratio. Computational fluid dynamics. Combustion chambers. High pressure. Dynamic tests.
Online Access:	https://purl.fdlp.gov/GPO/gpo133808