Low-speed wind-tunnel investigation of lateral control characteristics of a 60 degrees triangular-wing model having half-delta tip controls

Byron M. Jaquet, M. J. Queijo
naca-rm-l51i10
Nov 1951


A low-speed investigation was made in the Langley stability tunnel to determine the lateral control characteristics of a 60 degree triangular-wing model equipped with half-delta tip controls having areas of 5, 10, or 15 percent of the sing area (sum left-and right-control areas).

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http://naca.central.cranfield.ac.uk/reports/1951/naca-rm-l51i10.pdf