SST Technology Follow-On Program-Phase II. Flutter Studies of a Supersonic Transport Wing with Mass Balance.
Abstract
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.
Document Details
- Document Type
- Technical Report
- Publication Date
- Jul 01, 1973
- Accession Number
- AD0917345
Entities
People
- John R. Hogley
- Warren H. Weatherill
Organizations
- Boeing