Low speed aerodynamic characteristics of non-slender delta wing at low angles of attack

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 Mach number of 0.1 and angles of attack up to 25°, in...

Fuld beskrivelse

Bibliografiske detaljer

Principais autores:	Mohamed A. Mohamed, Imran Afgan, Mohamed Hefny Salim, Ibrahim K. Mohamed
Format:	Artigo
Sprog:	Inglês
Udgivet:	Elsevier 2022-12-01
Serier:	Alexandria Engineering Journal
Fag:	Non-slender delta wing Half-span Subsonic wind tunnel Surface pressure measurements Aerodynamic characteristics
Online adgang:	http://www.sciencedirect.com/science/article/pii/S1110016822001703
Tags:	Tilføj Tag Ingen Tags, Vær først til at tagge denne postø!