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The Convair 990 had particularly obvious anti-shock bodies; modern airliners usually have more subtle shaping for area ruling.
The Convair 990 had particularly obvious anti-shock bodies; modern airliners usually have more subtle shaping for area ruling.
NASA TF-8A in 1973
NASA TF-8A in 1973
Thomas McMurtry before his flight on the Vought F-8A Crusader Supercritical Wing Airplane
Thomas McMurtry before his flight on the Vought F-8A Crusader Supercritical Wing Airplane
Supercritical airfoil Mach number/pressure coefficient diagram (y axis: Mach number, or pressure coefficient, negative up; x axis: position along chor
Supercritical airfoil Mach number/pressure coefficient diagram (y axis: Mach number, or pressure coefficient, negative up; x axis: position along chord, leading edge left). The sudden increase in pressure coefficient at midchord is due to the shock.