S8  Engenharia Aeroespacial
 
 Title:
DESIGN METHOD OF CLOSED TEST SECTION
 
Summary :
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.  
 
Author :
Popescu, Theodor T.
Popescu, Daniela L.
 
 
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