COMPUTATIONAL SIMULATION OF COMPRESSIBLE FLOWS IN THE RAE 2822 AERODYNAMIC PROFILE
Investigation of shock-boundary layer interactions in supersonic axial turbines
Simulation of large scales and aeroacoustics of perfectly expanded supersonic jets
Grant number: | 98/10092-8 |
Support Opportunities: | Research Grants - Meeting - Abroad |
Start date: | September 28, 1998 |
End date: | October 05, 1998 |
Field of knowledge: | Engineering - Aerospace Engineering - Aerodynamics |
Principal Investigator: | Paulo Moraes Junior |
Grantee: | Paulo Moraes Junior |
Host Institution: | Instituto de Aeronáutica e Espaço (IAE). Departamento de Ciência e Tecnologia Aeroespacial (DCTA). Ministério da Defesa (Brasil). São José dos Campos , SP, Brazil |
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