Publication Date:
2006-02-14
Description:
Wall interference is made predominant in tunnel models and by wall geometries to facilitate the study of slot flow. The viscous effects in slots are studied by two dimensional measurements of flow. Wall interference is assessed by measuring pressure distributions at two levels near the walls. Interference on lifting delta wings is calculated. Pressure distributions at inner boundaries show basis axisymetries between the pressure side and the suction side, pointing to the necessity of having wider slots on the pressure side.
Keywords:
AERODYNAMICS
Type:
NASA. Langley Research Center Wind Tunnel Wall Interference Assessment and Correction, 1983; p 293-300
Format:
text
Permalink