Deflection of turbofan exhaust streams for enhanced engine/nacelle integration
Year: 1997
Type: conference-paper
DOI: 10.2514/6.1997-3152
Authors: R. Tindell, F. Marconi, I. Kalkhoran, J. Yetter
Institutions: Northrop Grumman (United States), Langley Research Center
Language: English
Subfield: Aerospace Engineering
Field: Engineering
Domain: Physical Sciences
Open Access status: closed
Funders: Northrop Grumman, Langley Research Center
OpenAlex ID: W2329328548
