Engineering methods to calculate unsteady airloads on wings in transonic flow were applied in flutter calculations for a semispan flutter model of a supercritical wing. A verification was performed by comparing flutter characteristics, and the prediction of transonic dips in the flutter boundaries. When applied complementary, the methods produce useful results.
Verification of Calculation Methods for Unsteady Airloads in the Precipitation of Transonic Flutter
1984
11 pages
Report
Keine Angabe
Englisch
Unsteady airloads in supercritical transonic flows
AIAA | 1979
|Unsteady Airloads in Supercritical Transonic Flows
AIAA | 1981
|