Previous report gave calculations for pressure distribution over thin oblique airfoils at supersonic speed; present report extends calculations to subsonic speeds; it is found that flows again can be obtained by superposition of elementary conical flow fields; in case of sweepback wing pressure distributions remain qualitatively similar at subsonic and supersonic speeds. See also Engineering Index 1946 p 23.
Subsonic flow over thin oblique airfoils at zero lift
Nat Advisory Committee Aeronautics -- Tech Note
1947
13 pages
7 Supp Plates
Report
English
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Subsonic Flow Over Thin Oblique Airfoils at Zero Lift
NTIS | 1948
|Subsonic Flow over Thin Oblique Airfoils at Zero Lift
NTRS | 1947
|Subsonic flow over thin oblique airfoils at zero lift
TIBKAT | 1947
|Subsonic flow over thin oblique airfoils at zero lift
NTRS | 1948
|Subsonic flow over thin oblique airfoils at zero lift
NTRS | 1976
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