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2000 | OriginalPaper | Chapter

The Linear Theory of a Lifting System Moving Close to the Ground

Author : Professor Kirill V. Rozhdestvensky

Published in: Aerodynamics of a Lifting System in Extreme Ground Effect

Publisher: Springer Berlin Heidelberg

Included in: Professional Book Archive

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To reduce a nonlinear formulation to the linear theory, one has to assume that the deflections of the surfaces of the wing, its vortex wake, and the ground, respectively, from horizontal planes y = h1 and y = 0 are small compared to the ground clearance h, i.e., 3.1$$\begin{array}{*{20}{c}} {\left| {{y_{u,l,w}} - h} \right| \ll h,}&{\left| {{y_g}} \right|} \end{array} \ll h.$$

previous chapter Problem Formulation for the Flow Past a Lifting Surface in Proximity to a Solid Boundary
next chapter Nonlinear Flow Problems for a Lifting System in the Extreme Ground Effect
Metadata
Title
The Linear Theory of a Lifting System Moving Close to the Ground
Author
Professor Kirill V. Rozhdestvensky
Copyright Year
2000
Publisher
Springer Berlin Heidelberg
Book
Aerodynamics of a Lifting System in Extreme Ground Effect

Print ISBN: 978-3-642-08556-7

Electronic ISBN: 978-3-662-04240-3

Copyright Year: 2000

DOI
https://doi.org/10.1007/978-3-662-04240-3_3

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