The NASA supercritical airfoil development program is summarized in a chronological fashion. Some of the airfoil design guidelines are discussed, and coordinates of a matrix of family related supercritical airfoils ranging from thicknesses of 2 to 18 percent and over a design lift coefficient range from 0 to 1.0 are presented.
NASA supercritical airfoils: A matrix of family-related airfoils
1990-03-01
Report
Keine Angabe
Englisch
Review of NASA supercritical airfoils
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