Numerical investigation on the effect of cowl angle in the supersonic intake performance
Year: 2025
Type: article
Source: The Aeronautical Journal
DOI: 10.1017/aer.2025.7
Institution: Motilal Nehru National Institute of Technology
Language: English
Subfield: Computational Mechanics
Field: Engineering
Domain: Physical Sciences
Open Access status: closed
OpenAlex ID: W4409114273
