Investigation indicates that, except at very low flow rates, static pressure losses increase and total pressure variations become more pronounced with increasing weight flow; smoothing and rounding leading edges of screen vanes caused marked decreases in static pressure loss coefficients and slightly improved total pressure patterns.
Investigation of pressure-loss characteristics of turbojet inlet screen
Nat Advisory Committee Aeronautics -- Tech Note
1947
7 pages
19 Supp sheets
Report
English
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