Methods by which aerodynamic characteristics of air foil may be calculated with sufficient accuracy for use in airplane design are described and developed; these methods for prediction are based on present aerodynamic theory and on empirical formulas derived from data obtained in N.A.C.A. variable-density wind tunnel at Reynolds Number corresponding approximately to full scale. Bibliography. (see also abstract in Mech. Eng., vol. 51, no. 11, Nov. 1929, p. 851)
The prediction of airfoil characteristics
Nat. Advisory Committee Aeronautics -- Report
1930
13 pages
17 Figs.
Report
English
© Metadata Copyright Elsevier B. V. All rights reserved.
The prediction of airfoil characteristics
NTRS | 1930
|The prediction of airfoil characteristics
TIBKAT | 1929
|prediction of iced airfoil aerodynamic characteristics
AIAA | 2016
|Prediction of Iced Airfoil Aerodynamic Characteristics (AIAA 2016-1547)
British Library Conference Proceedings | 2016
|Geometric airfoil characteristics
Engineering Index Backfile | 1942
|