Modified Target Pressure Distribution for Supersonic Natural Laminar Flow Wing Design
Year: 2024
Type: article
Source: AIAA Journal
DOI: 10.2514/1.j064474
Authors: Han Nie, Wen-Ping Song, Zhong-Hua Han
Institution: Northwestern Polytechnical University
Language: English
Subfield: Computational Mechanics
Field: Engineering
Domain: Physical Sciences
Open Access status: closed
Awards: G2832354939, G6238685976
OpenAlex ID: W4404106803