SST Technology Follow-On Program-Phase II. Flutter Studies of a Supersonic Transport Wing with Mass Balance.
Final rept. on Task 5,
BOEING COMMERCIAL AIRPLANE CO SEATTLE WA
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This report documents the effects of mass balance on the flutter characteristics of the SST 2707-300 wing. The mass balance is supported on a boom when it is ahead of the wing leading edge. The effects of the size and location of the mass and the boom flexibility on symmetric and antisymmetric flutter at high and low gross weight and subsonic and supersonic Mach number are reported.
- Transport Aircraft