Computer program calculates effects on lift and drag of blowing two jets over swept tapered wing at low subsonic speeds. Algorithm used in based on vortex lattice representation of wing lifting surface on line source-sink distribution to represent effects of exhaust jets.
Swept-tapered-wing aerodynamics
NASA Tech Briefs ; 1 , 1
01.03.1976
Sonstige
Keine Angabe
Englisch
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