A-Z-Leitfaden über Thermodynamik, Wärme- und Stoffübertragung und Strömungstechnik
Deutsch English Русский 中文 Português Español Français Über unser Angebot Redaktion Kontakt Zugriff Begell House

Themen

Thermopedia
Applikationen
Industriell
Brennstoffzellen Industrielle Wärmetechnik Kerntechnik Plasmaenergieumwandlung Solarenergie Verbrennungsanlagen Wärmetauscher  Luftfahrtanwendungen
de Aeroacoustics de Aeroelasticity
de Flutter Aeroelasticity Distribution of Mach number around a plate at M = 1.0 Distribution of Mach number around a plate at M = 1.06 Distribution of Mach number around a plate at M = 1.3 Distribution of Mach number around a plate at M = 1.82 and flow density 0.000245 Distribution of Mach number around the diverged plate at M = 0.91 Divergence of plate at M = 0.91 First millisecond of the vibration of the stiffened shell, which corresponds to the fuselage of a small passenger airplane; the strike falls on the intersection of the stiffeners Growth of the second natural mode of oscillations of a plate (M = 1.3) Plate oscillation mode at M = 1.0 (corresponds to a borderline state between divergence and single mode flutter) Plate oscillations at M = 1.39 (the process is chaotic, with no specific mode dominated) Plate oscillations at M = 1.82 and flow density 0.000245 Pure single mode flutter oscillations of a plate (M = 1.06) Vibrations of the crosswise stiffened shell, which corresponds to the fuselage of a small passenger airplane, excited by the strike, fallen on the cell center Vibrations of the isotropic unstiffened shell, which corresponds to the fuselage of a small passenger airplane under the point impulse, which is represented by the ball strike Vibrations of the shell, which corresponds to the fuselage of a small pasenger airplaine, with "smeared" stringers; the strike falls on the center of the span Vibrations of the shell, which corresponds to the fuselage of a small pasenger airplaine, with "smeared" stiffeners; both the stringers and frames are "smeared." Vibrations of the shell, which corresponds to the fuselage of a small passenger airplane, with "smeared" stringers; the strike falls on the frame Vibrations of the stiffened shell, which corresponds to the fuselage of a small passenger airplane; the strike falls on the intersection of the stiffeners
de Dynamics and Control de Flow control de Wind Tunnel Experiment  Triebwerke  Wärmeübertragung in Luftfahrtanwendungen
Menschliche Gesundheit Natur Technologien
Berechnungsverfahren Experimentelle Techniken Fachübergreifende Inhalte Fundamentaldaten

Hauptthemen

A-Z-Index Autoren / Redakteure Semantische Karte Visuelle Galerie Einen Beitrag leisten Guest