Results on NACA 4412 section indicate that pressure distribution is practicaly unaffected by changes in Reynolds Number except where separation is involved. (10¢)
Variations with Reynolds number of pressure distribution over airfoil section
Nat Advisory Committee Aeronautics -- Report
1938
20 pages
Bibliography
Report
English
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Variations with Reynolds number of pressure distribution over airfoil section
Engineering Index Backfile | 1938
|Variation, with Reynolds number, of pressure distribution over airfoil section
Engineering Index Backfile | 1938
|Airfoil section characteristics as affected by variations of Reynolds Number
Engineering Index Backfile
|Airfoil section characteristics as affected by variations of Reynolds Number
Engineering Index Backfile | 1937
|Airfoil section characteristics as affected by variations of Reynolds Number
Engineering Index Backfile | 1937
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