Application of the Adjoint Method to an Unstructured Subsonic/Supersonic Panel Method
Year: 2025
Type: article
Source: Journal of Aircraft
DOI: 10.2514/1.c038478
Institution: Utah State University
Language: English
Subfield: Computational Mechanics
Field: Engineering
Domain: Physical Sciences
Open Access status: closed
OpenAlex ID: W4414396289
