Camada limite de temperatura com gradiente de pressão adverso

• Ano de defesa: 1976
• Autor(a) principal: Oliveira, Márcio Valério
• Tipo de documento: Dissertação
• Tipo de acesso: Acesso aberto
• Idioma: por
• Instituição de defesa: Universidade Federal do Rio de Janeiro; Brasil; Instituto Alberto Luiz Coimbra de Pós-Graduação e Pesquisa de Engenharia; Programa de Pós-Graduação em Engenharia Mecânica; UFRJ
• Palavras-chave em Português: Queda de pressão; Equações integrais; Transferência de calor; CNPQ::ENGENHARIAS::ENGENHARIA MECANICA::FENOMENOS DE TRANSPORTE::TRANSFERENCIA DE CALOR
• Link de acesso: http://hdl.handle.net/11422/3551

The Prandtl's boundary layer energy equation has been solved by integral methods using a polinomial biparametric velocity profile with variable exponent as suggested by Geropp and a temperature profile presented by Van Driest which is modified to consider the presence of the pressure gradient. The compressible laminar boundary layer in an adverse pressure gradient is analyzed on the basis of the momentum and thermal integral equations. A method of calculating the boundary layer as function of the Mach number, uniform wall temperature and finite suction distribution is developed. The results obtained agree with the availables exact soluctions and the accurate approximate methods using different approach to solve the heat transfer problem and show that the solution of the thermal energy equation with the parametric correction of the pressure and temperature gradient are a mathematically simple and fast way to solve that problem.