Transonic Flow at a Slotted Test Section Wall.
Interim scientific rept. 1 Oct 71-30 Sep 72,
AERONAUTICAL RESEARCH INST OF SWEDEN STOCKHOLM
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The aim is to arrive at a better understanding of the structure of slot flow under different conditions inflow, outflow, presence of wall boundary layers, etc. in order to compute wall corrections with required accuracy. As a first step towards this end, using simple and available tools, the investigation is concerned with 1 Experimental study of slot flow in a small transonic wind tunnel 2 Elementary theoretical analysis of slot flow with a schematic boundary layer 3 Numerical computation of near-sonic flow in a slotted test section using simplified boundary conditions. Author
- Test Facilities, Equipment and Methods