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Lattice arrangements for rapid convergence Vortex-Lattice Utilization Vortex-Lattice Utilization (1926)
NASA Technical Reports Server (NTRS) · leaf 14
Se ee 2 d, INSET DISTANCE {Vee 2.85 0 2.80 LIFT-CURVE SLOPE, Cy, 4 CHORDWISE VORTICES 2.75 2. 709 0.04 0.08 0.12 0.16 (NUMBER OF SPANWISE VORTICES)~1 Figure 7.- Lift-curve slope convergence for tapered wing. WARREN.12 PLANFORM, 10 SPANWISE VORTICES FAR FIELD CALCULATION- 1.02 1.00 E ccranoutan… … Figure 8.- Induced drag for tapered wing. 339NASA Technical Reports Server (NTRS) · Hough · Legacy CDMS · Vought Corp
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