Article
Article
- Engineering & Materials
- Aeronautical engineering
- Low-speed aircraft
- Physics
- Fluid mechanics
- Low-speed aircraft
DISCLAIMER: This article is being kept online for historical purposes. Though accurate at last review, it is no longer being updated. The page may contain broken links or outdated information.
Low-speed aircraft
Article By:
DeLaurier, James D. Institute for Aerospace Studies, University of Toronto, Ontario, Canada.
Last reviewed:2005
DOI:https://doi.org/10.1036/1097-8542.YB050750
- Boundary-layer flow
- Laminar separation bubble
- Low-speed flight
- Related Primary Literature
- Additional Reading
It might be thought that low-speed small-scale aircraft are simply smaller versions of full-scale designs and that textbook aerodynamics apply to them. However, low-speed aircraft have very special lift and drag characteristics that distinguish them from their higher-speed counterparts. To a large measure, this is determined by a key nondimensional parameter called the Reynolds number (Re). It was derived from water-pipe experiments by Professor Osborne Reynolds at the University of Manchester over 100 years ago, but the concept has found crucial application in aerodynamics. For such a powerful parameter, the Reynolds number has a very simple form, as seen below,
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