The predicted effect of aerodynamic detuning of coupled bending-torsion unstalled supersonic flutter
By: Daniel Hoyniak and Sanford Fleeter.
Contributors: Fleeter, Sanford.; Lewis Research Center.
Series: NASA technical memorandum -- 87240.
Publisher: National Aeronautics and Space Administration, Lewis Research Center
Published: 1986
Place of publication: [Cleveland, Ohio
Language: eng
Format: Microform
Subjects: Flutter (Aerodynamics); Aerodynamics, Supersonic.; Bending.; Coupled modes.; Rotor blades (turbomachinery); Supersonic flutter.; Torsion.; Tuning.
Notes: Microfiche. [Washington, D.C. : National Aeronautics and Space Administration], 1986. 1 microfiche.