Research Catalog

Aeroelasticity and structural optimization of composite helicopter rotor blades with swept tips

Title
Aeroelasticity and structural optimization of composite helicopter rotor blades with swept tips [microform] / K.A. Yuan and P.P. Friedmann.
Author
Yuan, K. A.
Publication
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1995]

Details

Additional Authors
Langley Research Center.
Description
1 v.
Series Statement
NASA contractor report ; 4665
Uniform Title
NASA contractor report ; NASA CR-4665.
Subject
  • Aerodynamic loads
  • Aeroelasticity
  • Composite structures
  • Dynamic response
  • Finite element method
  • Floquet theorem
  • Hamiltonian functions
  • Helicopters
  • Mathematical models
  • Rotary wings
  • Structural analysis
Note
  • Distributed to depository libraries in microfiche.
  • Shipping list no.: 95-0748-M.
Reproduction (note)
  • Microfiche.
Call Number
READEX Microfiche NAS 1.26:4665
OCLC
marcive33412559
Author
Yuan, K. A.
Title
Aeroelasticity and structural optimization of composite helicopter rotor blades with swept tips [microform] / K.A. Yuan and P.P. Friedmann.
Imprint
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
Series
NASA contractor report ; 4665
NASA contractor report ; NASA CR-4665.
Reproduction
Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1995] 5 microfiches.
Added Author
Langley Research Center.
Gpo Item No.
0830-H-14 (MF)
Sudoc No.
NAS 1.26:4665
Research Call Number
READEX Microfiche NAS 1.26:4665
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