Flutter at supersonic speeds : derivative coefficients for a thin aerofoil at zero incidence
1949
35 S.
graph. Darst.
Langzeitarchivierung durch Technische Informationsbibliothek (TIB) / Leibniz-Informationszentrum Technik und Naturwissenschaften und Universitätsbibliothek
Report
Englisch
Aerofoil theory of a flat delta wing at supersonic speeds
TIBKAT | 1952
|Flutter of multibay panels at supersonic speeds
AIAA | 1964
|Active control of aerofoil flutter
AIAA | 1987
|