Guia A a Z para Thermodinâmicas, Transferência de calor e massa, e Engenharia de Fluidos
Português English Русский 中文 Español Français Deutsch Sobre Editores Contato Acesso Begell House

Temas

Thermopedia
Aplicações
Industrial
Aplicações Aeroespaciais
Motores pt Aeroacoustics pt Aeroelasticity
pt 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
pt Dynamics and Control pt Flow control pt Wind Tunnel Experiment Transferência de calor em aplicações aeroespaciais
Células Combustíveis Conversão de Energia em Plasmas Energia Solar Engenharia Nuclear Engenharia Térmica Industrial Sistemas de Combustão Trocadores de Calor
Natureza Saúde Humana Tecnologias
Conteúdo Interdisciplinar Fundamentos Métodos Computacionais Técnicas Experimentais

Principais Tópicos

Índice A-Z Autores / Editores Mapa semântico Galeria Visual Contribuir Guest