Stresses and rate of twist in single-cell thin-walled beams with anisotropic walls

AIAA Journal

Volumn 26, Issue 9, 1988, Pages 1107-1118

  Libove, Charles ^a  

^a SYRACUSE UNIVERSITY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT MATERIALS; COMPOSITE MATERIALS--STRESSES; LAMINATED PRODUCTS--AEROSPACE APPLICATIONS; STRESSES--ANALYSIS; TUBES;

AEROSPACE STRUCTURES; BENDING; ELASTIC THIN WALLED BEAMS; RATE OF TWIST; SHEAR FLOWS; SHEAR STRAIN;

BEAMS AND GIRDERS;

EID: 0024071882     PISSN: 00011452     EISSN: None     Source Type: Journal    
DOI: 10.2514/3.10018     Document Type: Article

References (8)

1. Kuhn, P., Stresses in Aircraft and Shell Structures, McGraw-Hill, New York, 1956, Chap. 2.
2. Rivello, R. M., Theory and Analysis of Flight Structures, McGraw-Hill, New York, 1969, Chap. 9.
3. Bruhn, E. F., Analysis and Design of Flight Vehicle Structures, F. R. F. Jacobs Associates, Carmel, IN, 1973, Chaps. A19 and A20.
4. Timoshenko, S. P. and Goodier, J. N., Theory of Elasticity, 3rd ed., McGraw-Hill, New York, 1970, p. 333.
5. Mansfield, E. H. and Sobey, A. J., “The Fiber Composite Helicopter Blade,” Aeronautical Quarterly, May 1979, pp. 413-449.
6. Rehfield, L. W., “Design Analysis Methodology for Composite Rotor Blades,” Seventh DOD/NASA Conference on Fibrous Composites in Structural Design, June 1987.
7. Chang, S. I., “Numerical Studies of Stresses and Deformations in Single-Cell Thin-Walled Beams with Anisotropic Walls,” MS Thesis, Dept, of Mechanical and Aerospace Engineering, Syracuse Univ., Syracuse, NY, March 1988.
8. Chang, S. I. and Libove, C., “Shear Flows, Strains and Rate of Twist in Single-Cell Thin-Walled Beams with Anisotropic Composite Walls: Simple Theory Compared with NASTRAN and Experiment,” presented at the Composite Materials session of the ASME Winter Annual Meeting in Chicago, Nov. 28-Dec. 2, 1988.