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S8 Engenharia Aeroespacial |
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Titulo:
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DESIGN METHOD OF CLOSED TEST SECTION
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Resumo :
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ABSTRACT: A DESIGN METHOD OF THE CLOSED TEST SECTION FOR SUBSONIC WIND TUNNELS IS PRESENTED. THE GOVERNING EQUATION INVOLVED IS THE INTEGRO-DIFFERENTIAL FORM OF THE MOMENTUM EQUATION. THE METHOD IS APPLIED TO THE RECTANGULAR AND CIRCULAR TEST SECTION. A NUMERICAL EXAMPLE IS ACHIEVED.
KEYWORDS: CLOSED TEST SECTION, WIND TUNNEL.
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Autores :
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Popescu, Theodor T.
Popescu, Daniela L.
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Trabalho Completo :
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