Note on the effect of compressibility on the profile drag of aerofoils at subsonic Mach numbers in the absence of shock waves
1950
16 S.
graph. Darst.
Langzeitarchivierung durch Technische Informationsbibliothek (TIB) / Leibniz-Informationszentrum Technik und Naturwissenschaften und Universitätsbibliothek
Report
Englisch
Theoretical critical mach numbers for NACA16 series aerofoils
TIBKAT | 1945
|Engineering Index Backfile | 1947
|The calculation of the profile drag of aerofoils
TIBKAT | 1937
|The calculation of the profile drag of aerofoils
SLUB | 1937
|