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Chordwise and spanwise loadings measured at low speed on large triangular wings
Adrien E Anderson
Open publisher page 2 citations
Abstract
Report presenting pressure distributions of three triangular wing models: a wing-alone model, the same wing combined with a body, and a mock-up of a triangular-wing airplane. Results regarding the separation-vortex air flow over triangular wings, general comments regarding the applicability of the study, chordwise pressure distribution, section lift characteristics, center of pressure, and span load distribution are provided.