An oscillating wing with control surfaces in two-dimensional, compressible, subsonic flow is investigated. Computed numerical results are given for the forces and moments, useful for flutter calculations.
Zur Stabilitaet des schwingenden Tragfluegels im Unterschallbereich (Stability of an Oscillating Wing in Subsonic Range)
1969
9 pages
Report
Keine Angabe
Englisch
Aerodynamische Beiwerte des elliptischen Tragfluegels
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