Analysis of unswept and swept wing chordwise pressure data from an oscillating naca 0012 airfoil experiment : vol. - I : technical report

Analysis of unswept and swept wing chordwise pressure data from an oscillating naca 0012 airfoil experiment : vol. - I : technical report - - Washington, D.C. NASA 1983 - 104 p. - NASA CR 3567 : 1983 .





Aerodynamic testing, Airfoil aerodynamics, Dynamic stall, Oscillating NACA 0012 airfoil, Pitching oscillations

LNASA CR 3567 : 1983

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