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Comment on “Thickness and Camber Effects in Slender Wing Theory
Citation
Laverón Simavilla, Ana and Perales Perales, José Manuel (2005). Comment on “Thickness and Camber Effects in Slender Wing Theory. "AIAA Journal", v. 43 (n. 11); p. 2462. ISSN 0001-1452. https://doi.org/10.2514/1.7530.
Description
| Title: | Comment on “Thickness and Camber Effects in Slender Wing Theory |
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| Author/s: |
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| Item Type: | Article |
| Título de Revista/Publicación: | AIAA Journal |
| Date: | November 2005 |
| ISSN: | 0001-1452 |
| Volume: | 43 |
| Subjects: | |
| Faculty: | E.U.I.T. Aeronáutica (UPM) |
| Department: | Vehículos Aeroespaciales [hasta 2014] |
| Creative Commons Licenses: | Recognition - No derivative works - Non commercial |
Abstract
IN the paper by Plotkin,1 first-order corrections to slender wing theory2 were developed due to spanwise thickness and camber distributions. The velocity potential <f>(x, y, z) calculated in the paper1 actually corresponds to the flow having zero normal velocity at the body contour and a vertical velocity at infinity proportional to the angle of attack [<f>z(x, y, \z\ -> oo) = Ua]
More information
| Item ID: | 4916 |
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| DC Identifier: | https://oa.upm.es/4916/ |
| OAI Identifier: | oai:oa.upm.es:4916 |
| DOI: | 10.2514/1.7530 |
| Official URL: | http://www.aiaa.org/content.cfm?pageid=406&gTable=... |
| Deposited by: | Memoria Investigacion |
| Deposited on: | 11 Nov 2010 09:36 |
| Last Modified: | 20 Apr 2016 13:56 |
