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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Abstract
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 |
| URI: | http://nal-ir.nal.res.in/id/eprint/1944 |
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