Approximate linearized solution is obtained from source distribution about cylinder and is accurate for limiting case of ring airfoils having small chord-radius ratios.
Theoretical wave drag and lift of thin supersonic ring airfoils
Nat Advisory Committee Aeronautics -- Tech Note
1948
20 pages
Report
English
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Theoretical wave drag and lift of thin supersonic ring airfoils
TIBKAT | 1948
|Maximum lift-to-drag ratio airfoils at moderate supersonic speeds
Engineering Index Backfile | 1969
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