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Accession Number:
AD0623740
Title:
NONUNIFORM STEADY FLOW OF AN IDEAL FLUID PAST AIRFOILS. PART III. NUMERICAL RESULTS.
Corporate Author:
MATHEMATICS RESEARCH CENTER UNIV OF WISCONSIN MADISON
Report Date:
1965-07-01
Abstract:
In Parts I and II AD-610 445 and AD-614 929 theories for nonuniform flow of an exponential type past airfoils were derived. In this part a further improvement to the approximate theory of Part II is developed. The velocity distribution at elliptical profiles of relative thickness 0.1 and 0.2 was computed for angles of attack in the range 0 or sin alpha or 0.3 and is shown in tables in such a way that the accuracy of the methods can easily be compared. Author
Descriptive Note:
Technical summary rept.,
Pages:
0039
Contract Number:
DA-11-022-ORD-2059
File Size:
0.00MB
