Aeroelasticity and structural optimization of composite helicopter rotor blades with swept tips
By: K.A. Yuan and P.P. Friedmann.
Contributors: Langley Research Center.
Series: NASA contractor report -- 4665.; NASA contractor report -- NASA CR-4665.
Publisher: National Aeronautics and Space Administration, Langley Research Center; National Technical Information Service, distributor
Published: 1995
Place of publication: Hampton, Va; [Springfield, Va
Language: eng
Format: Microform
Subjects: Aerodynamic loads.; Aeroelasticity.; Composite structures.; Dynamic response.; Finite element method.; Floquet theorem.; Hamiltonian functions.; Helicopters.; Mathematical models.; Rotary wings.; Structural analysis.
Notes: Distributed to depository libraries in microfiche.

Shipping list no.: 95-0748-M.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1995] 5 microfiches.