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Journal ArticleDOI

Note on an airfoil in a slightly non-uniform stream

Allan J. Acosta, +1 more
- 01 Aug 1968 - 
- Vol. 18, Iss: 1, pp 21-27
TLDR
In this article, the modifications that must be made to two-dimensional calculations of the flow past an airfoil when the flow takes place in a symmetric channel with slightly non-parallel walls are investigated.
Abstract
An investigation is presented of the modifications that must be made to two-dimensional calculations of the flow past an airfoil when the flow takes place in a symmetric channel with slightly non-parallel walls.

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References
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Journal ArticleDOI

Tables of Integrals

J Crank
- 01 Jun 1962 - 
TL;DR: In the fourth edition of the book as mentioned in this paper, the section on definite integrals has been considerably enlarged and a section added on integrals essentially of elliptic type, which is the case with the present edition.

Second-order subsonic airfoil theory including edge effects

Milton D
TL;DR: In this paper, a unified second-order theory for airfoil sections of arbitrary shape is proposed, and the solution is reached in three steps: the incompressible result is found by integration, it is converted into the corresponding subsonic compressible result by means of the secondorder compressibility rule, and it is rendered uniformly valid near stagnation points by further rules.