A Decoupled Method for Estimating Non-Ideal Sonic Boom Performance of Low-Boom Aircraft Due to Off-Design Flight Conditions and Non-Standard Atmospheres
Year: 2021
Type: conference-paper
Source: AIAA SciTech Forum
DOI: 10.2514/6.2021-1271
Institutions: Boeing (United States), Texas A&M University
Language: English
Subfield: Computational Mechanics
Field: Engineering
Domain: Physical Sciences
Open Access status: closed
OpenAlex ID: W3119002060
