Effect of reflex camber on the aerodynamic characteristics of a highly tapered moderately swept-back wing at Reynolds numbers up to 8,000,000
1947
10, [7] S
Ill., graph. Darst
Langzeitarchivierung durch Technische Informationsbibliothek (TIB) / Leibniz-Informationszentrum Technik und Naturwissenschaften und Universitätsbibliothek
Buch
Englisch
Engineering Index Backfile | 1947
|Reynolds number effects on flow characteristics and aerodynamic performances of a swept-back wing
Online Contents | 2011
|