Aeroelastic tailoring of forward swept composite wings

Journal of Aircraft

Volumn 18, Issue 8, 1981, Pages 669-676

  Weisshaar, Terrence A ^a,b  

^a PURDUE UNIVERSITY   (United States)

^b Schools of Aeronautics and Astronautics Chemical and Materials Engineering   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS;

EID: 0019597865     PISSN: 00218669     EISSN: None     Source Type: Journal    
DOI: 10.2514/3.57542     Document Type: Article

References (14)

1. Krone, N. J. Jr., “Divergence Elimination with Advanced Composites,” AIAA Paper 75-1009, 1975.
2. Weisshaar, T. A., “Divergence of Forward Swept Composite Wings,” Journal of Aircraft, Vol. 17, June 1980, pp. 442-448.
3. Stroud, W. J., “Automated Structural Design with Aeroelastic Constraints: A Review and Assessment of the State of the Art,” Paper presented at Structural Optimization Symposium, ASME Winter Meeting, New York, 1974.
4. Shirk, M. H. and Griffin, K. E., “The Role of Aeroelasticity in Aircraft Design with Advanced Filamentary Composite Materials,” Paper presented at Second Conference on Fibrous Composites in Flight Vehicle Design, Dayton, Ohio, May 1974.
5. Diederich, F. W. and Foss, K. A., “Charts and Approximate Formulas for the Estimation of Aeroelastic Effects on the Loading of Swept and Unswept Wings,” NACATN 2608, Sept. 1951.
6. Weisshaar, T. A., “Aeroelastic Stability and Performance Characteristics of Aircraft with Advanced Composite Sweptforward Wing Structures,” AFFDL-TR-78-116, Sept. 1978.
7. Tsai, S. W. and Hahn, H. T., Introduction to Composite Materials, Technomic Publishing Co., Inc., Westport, Conn., 1980.
8. Weisshaar, T. A., “Forward Swept Wing Static Aeroelasticity,” AFFDL-TR-79-3087, June 1979.
9. Gray, W. L. and Schenk, K. L., “A Method for Calculating the Subsonic Steady-State Loading on an Airplane with a Wing of Arbitrary Plan Form and Stiffness,” NACA TN 3030, July 1953.
10. Sobieski, J., private communication, NASA/Langley Research Center, Nov. 1979.
11. Bisplinghoff, R. L., Ashley, H., and Halfman, R. L., Aeroelasticity, Addison-Wesley, Reading, Mass., 1955, pp. 506-509.
12. Lynch, R. W. and Rogers, W. A., “Aeroelastic Tailoring of Composite Materials to Improve Performance,” Proceedings of the AIAA/ASME/SAE 17th Structures, Structural Dynamics and Materials Conference, 1976, pp. 61-79.
13. Hertz, T. J., Shirk, M. H., Ricketts, R. H., and Weisshaar, T. A., “Aeroelastic Tailoring with Composites Applied to Forward Swept Wings,” Proceedings of the 5th DOD/NASA Conference on Fibrous Composites in Structural Design, Jan. 1981.
14. Jones, R. M., Mechanics of Composite Materials, McGraw-Hill Book Co., 1975, pp. 45-59.