A Shortened Method for the Calculation of Aerofoil Profile Drag-Reference-Cited by-同舟云学术

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A Shortened Method for the Calculation of Aerofoil Profile Drag

Published:1952-02 Issue:494 Volume:56 Page:109-116
ISSN:0368-3931
Container-title:The Journal of the Royal Aeronautical Society
language:en
Short-container-title:J. R. Aeronaut. Soc.

Author:

Dowlen E. M.

Abstract

SummaryA rapid method is developed for estimating the profile drag of an aerofoil with a known transition point position. The results are in good agreement with previous calculations.

Publisher

Cambridge University Press (CUP)

Reference5 articles.

1. Tetervin Neal (1944). A Method for the Rapid Estimation of Turbulent Boundary Layer Thickness for Calculating Profile Drag. N.A.C.A. A.C.R. L4G14 (1944), A.R.C. 8498.

2. Squire H. B. and Young A. D. (1937). The Calculation of the Profile Drag of Aerofoils. R. & M. 1838, 1937.

3. Winterbottom N. E. and Squire H. B. (1940). Note on Further Wing Profile Drag Calculations. R.A.E. Report B.A. 1634, 1940.

4. Lock R. C. (1948). Note on Profile Drag Calculations for Low-Drag Wings with Cusped Trailing Edges. R.A.E. Report Aero. 2130 and Corrigenda, 1948.

5. Young A. D. (1948). Skin Friction in the Laminar Boundary Layer in Compressible Flow. College of Aeronautics Report No. 20, 1948.

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1. Convective Heat Transfer to Gas Turbine Blade Surfaces;Proceedings of the Institution of Mechanical Engineers;1954-06

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