Analysis, Design, and Optimization of Noncylindrical Fuselage for Blended-Wing-Body Vehicle
Year: 2004
Type: article
Source: Journal of Aircraft
DOI: 10.2514/1.417
Institution: Langley Research Center
Language: English
Subfield: Aerospace Engineering
Field: Engineering
Domain: Physical Sciences
Open Access status: closed
Funder: Boeing
OpenAlex ID: W2166589487
