Effect of compressive force on strut-braced wing response

19th AIAA Applied Aerodynamics Conference

Volumn , Issue , 2001, Pages

  Sulaeman, Erwin ^a   Kapania, Rakesh K ^a   Haftka, Raphael T ^b  

^a Virginia Polytechnic Institute and State University   (United States)

^b J Crayton Pruitt Family Department of Biomedical Engineering   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; BUCKLING; DESIGN AIDS; EIGENVALUES AND EIGENFUNCTIONS; STIFFNESS; STIFFNESS MATRIX;

AERODYNAMIC LOAD DISTRIBUTIONS; AEROELASTIC RESPONSE; COMPRESSIVE FORCES; COMPUTATIONALLY EFFICIENT; EIGENVALUE ANALYSIS; GEOMETRIC STIFFNESS; MULTIDISCIPLINARY DESIGN OPTIMIZATION; STRUCTURAL RESPONSE;

STRUTS;

EID: 85067318184     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2001-1611     Document Type: Conference Paper

References (24)

1. th AIAA Aerospace Sciences Meeting and Exhibit, Reno, NV, January 10-13, 2000.
2. Gern, F.H., Gundlach, J.F., Ko, A., Naghshineh-Pour, A., Sulaeman, E., Tetrault P.A., Grossman, B., Haftka, R.T., Kapania R.K., Mason, W.H, and Schetz, J.A., Multidisciplinary Design Optimization of a Transonic Commercial Transport with a Strut-Braced Wing, SAE 1999-01-5621, 1999 World Aviation Congress, San Francisco, CA, Oct. 19-21, 1999.
3. Naghshineh-Pour, A., Structural Optimization and Design of a Strut-Braced Wing Aircraft, MS Thesis, Virginia Tech, November 1998.
4. s' AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference and Exhibit, Atlanta, GA, April 3-6,2000.
5. Ko, A., Mason, W.H., Grossman, B., and Haftka, R.T., Effects of Constraints in the Multidisciplinary Design Optimization of a Transonic Commercial Transport with a Strut-Braced Wing, 2001 World Aviation Congress, San Francisco, CA, October 2001.
6. rd ed., Van Nostrand Reinhold, New York, 1990.
7. Yang, T.Y., Finite Element Structural Analysis, Prentice Hall, 1986.
8. Gallagher, R.H., and Lee, C.H., Matrix Dynamic and Instability Analysis with non-uniform Elements, International Journal for Numerical Methods in Engineering, Vol. 20, No. 2, 1970.
9. Lee, S.Y., Ke, H.Y., and Kuo, Y.H., Exact Static Deflections of a Non-Uniform Bernoulli-Euler Beam with General Elastic End Strains, Computers and Structures, Vol. 36, No. 1, 1990, pp. 91-97.
10. Banerjee, J.R., and Williams, F.W., Exact Bernoulli-Euler Static Stiffness Matrix for a Range of Tapered Beam-Columns, International Journal for Numerical Methods in Engineering, Vol. 23, 1986, pp. 1615-1628.
11. Friedman, Z., and Kosmatka, J.B., Exact Stiffness Matrix of a Non-Uniform Beam, Computers and Structures, Vol. 42, 1992, pp. 671-682.
12. Mou, Y. Han, R.P.S.,and Shah A.H, Exact Dynamic Stiffness Matrix for Beams of Arbitrarily Varying Cross Sections, International Journal for Numerical Methods in Engineering Vol. 40, No. 2, 1997, pp.233-250.
13. Ábrate, S., Vibration of Non-Uniform Rods and Beams, Journal of Sound and Vibration, Vol.204, No. 4, 1995, pp. 703-716.
14. H.Kumar, B.M., and Sujith, R.I., Exact Solutions for Longitudinal Vibration of Non-Uniform Rods, Journal of Sound and Vibration, Vol.206, No. 5, 1997, pp. 721-729.
15. Eisenberger, M., Exact Longitudinal Vibration Frequency of a Variable Cross-section Rods, Applied Acoustics, Vol. 34, No. 2, 1991, pp. 123-130.
16. Ló Eisenberger M., An Exact Element Methods, International Journal for Numerical Methods in Engineering, Vol. 30, No. 2, 1990, pp. 363-370.
17. Iremonger, M.J., Finite Difference Buckling Analysis of Non-Uniform Columns, Computers and Structures, Vol. 12, 1980, pp. 741-748.
18. Von Karman, T., Biot, M.A., Mathematical Method in Engineering, McGraw-Hill, New York, 1940, pp. 306-309.
19. Karabalis, D.L., and Beskos, D.E., Static, Dynamic and Stability Analysis of Structures Composed of Tapered Beams, Computers and Structures, Vol. 16, No. 6, 1983, pp. 731-748.
20. Rodden, W. P., and Johnson, E.H., MSC/ NASTRAN Aeroelastic Analysis, Version 68, 1994.
21. Vanderplaats Research and Development, Inc., DOT User's Manual, Version 4.20, Colorado Springs, CO, 1995.
22. Sulaeman, E. Aeroelastic Stability Analysis with a Geometric Stiffness Effect of a Strut-Braced Wing, PhD. Dissertation, Virginia Tech.,July 2001.
23. Wolfram, S., Mathematica, Fourth Ed., Cambridge University Press, 1999.
24. Blair, M., Moorhouse, D., and Weisshaar, T.A., System Design Innovation Using Multidisciplinary Optimization and Simulation, AIAA-2000-4705, 2000.