Zobrazeno 1 - 1
of 1
pro vyhledávání: '"Ibrahim K. Mohamed"'
Publikováno v:
Alexandria Engineering Journal, Vol 61, Iss 12, Pp 9427-9435 (2022)
Low-speed wind tunnel experiments are conducted to study the aerodynamic performance of a half-span delta wing with 45° leading-edge sweep at subsonic flow regime. The experiments are carried out at a Reynolds number of 8.37 × 105, a free-stream Ma
Externí odkaz:
https://doaj.org/article/4563b7359e2f4166b4ddba5ade9605ad
