Analysis of wings with spanwise multi-segmented flaps

Rajeswari, Ramamurthy S and Dutt, HNV and Holla, VS and Swamy, MS (1992) Analysis of wings with spanwise multi-segmented flaps. Journal of Aeronautical Society of India, 45 (2). pp. 143-151.

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A vortex lattice method has been developed to analyse simple, swept, tapered wings with spanta ise segmented flaps at both leading and trailing edges . Classical planar horse shoe vortex is used as the basic solution to the governing Laplace's equation . Compressibility corrections (ire accounted for using Prandil-Glauert analogy modified as applicable to wins with deflected flaps. Extensive numerical experimentation has been carried to detcrinine the optin/um lattice layout. The method has been validated using a number of test cases available in published literature

Item Type: Article
Uncontrolled Keywords: Wings;Spanwise;Multi-segmented;Flaps
Subjects: AERONAUTICS > Aeronautics (General)
Depositing User: Ms Indrani V
Date Deposited: 25 Jul 2006
Last Modified: 01 Sep 2015 09:24

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