Second-order supercavitating hydrofoil theory
Open Access
- 1 May 1962
- journal article
- research article
- Published by Cambridge University Press (CUP) in Journal of Fluid Mechanics
- Vol. 13 (3), 321-332
- https://doi.org/10.1017/s0022112062000749
Abstract
The second-order problem of Helmholtz flow past lifting hydrofoils and symmetric struts has been formulated and solved. The solution involves elementary operations on the known solutions of the first-order problem. The second-order lift and drag coefficients are given in integral form. Results obtained for a flat plate at incidence and a symmetric wedge agree with the exact solutions up to the second order. In terms of quantitative improvements, the present second-order theory predicts a lift coefficient for a flat plate at 45° incidence with an error of 8%, and a drag coefficient for a symmetric wedge of 50° included angle with an error of 5%; the corresponding angles at which the linear theory would predict force coefficients incurring the same errors are 5° and 15° respectively.Keywords
This publication has 4 references indexed in Scilit:
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- LINEARIZED THEORY FOR FLOWS ABOUT LIFTING FOILS AT ZERO CAVITATION NUMBERPublished by Defense Technical Information Center (DTIC) ,1955
- Generalizations of the Inversion Formula of Thin Airfoil TheoryIndiana University Mathematics Journal, 1954
- A New Approach to Thin Aerofoil TheoryAeronautical Quarterly, 1951