NASA Technical Reports Server (NTRS) : Effect pdf

NASA Technical Reports Server (NTRS) : Effect

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Description of the Book:

Pressure and spanwise load distributions on a first-generation jet transport semispan model at subsonic speeds are presented. The wind tunnel data were measured for the wing with and without an alternate winglet. The results show that the winglet affected outboard wing pressure distributions and increased the spanwise loads near the tip

• Creator/s: NASA Technical Reports Server (NTRS
• Date: 12/1/1978
• Year: 1978
• Book Topics/Themes: NASA Technical Reports Server (NTRS), JET AIRCRAFT, PRESSURE DISTRIBUTION, SEMISPAN MODELS, WINGLETS, AERODYNAMIC LOADS, LOAD DISTRIBUTION (FORCES), SUBSONIC SPEED, TRANSPORT AIRCRAFT, WIND TUNNEL TESTS, Montoya, L. C., Flechner, S. G., Jacobs, P. F

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