By use of theoretical treatment indicated by PRANDTL, it has been possible to generalize available experimental results so that predictions can be made of important wake parameters in terms of distance behind airfoil trailing edge and profile drag coefficient; method of application of theory to design of airplane is demonstrated.
Downwash and wake behind plain and flapped airfoils
Nat Advisory Committee Aeronautics -- Report
1939
28 pages
Bibliography
Report
Englisch
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Design charts for predicting downwash angles and wake characteristics behind plain and flapped wings
Engineering Index Backfile | 1939
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