Nonlinear aeroelastic analysis for a wrinkling aeroshell/ballute system

Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference

Volumn , Issue , 2010, Pages

  Wang, Z ^a   Yang, S ^a   Liu, D D ^a   Wang, X Q ^b   Mignolet, M P ^b   Bartels, Robert E ^c  

^a ZONA TECHNOLOGY INC   (United States)

^b AZ 85281   (United States)

^c NASA LANGLEY RESEARCH CENTER   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; COMPUTATIONAL FLUID DYNAMICS; FLOW OF GASES; NONLINEAR ANALYSIS; REENTRY; STATIC ANALYSIS; STRUCTURAL DYNAMICS; TRANSIENT ANALYSIS; WIND TUNNELS;

AERODYNAMIC TOOLS; DYNAMIC CHARACTERISTICS; DYNAMIC PRESSURES; HYPERSONIC RE-ENTRY; NON-LINEAR FINITE ELEMENTS; NONLINEAR AEROELASTIC ANALYSIS; SHOCK-SHOCK INTERACTIONS; WIND TUNNEL TESTS;

AEROELASTICITY;

EID: 84855635330     PISSN: 02734508     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2010-2879     Document Type: Conference Paper

References (18)

1. Scott, R.C., Bartels, R. E., and Kandil, O. A. An Aeroelastic Analysis of a Thin Flexible Membrane. in 48th AIAA/ASME/AHS/ASC Structures, Structural Dynamics, and Materials Conference. 2007. Honolulu, Hawaii.AIAA 2007-2316.
2. Rohrschneider, R.R., Variable-fidelity Hypersonic Aeroelastic Analysis of Thin-film Ballute for Aerocapture, in School of Aerospace Engineering. 2007, Georgia Institute of Technology.
3. Liu, D.D., Wang, Z., Yang, S., Cai, C., Wang, X., and Mignolet, M. Nonlinear Aeroelastic Methodology for A Membrane-on-Ballute Model with Hypersonic Bow Shock. in 50th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials. 2009. Palm Springs, California.AIAA-2009-2363.
4. Wagner, H., Flat Sheet Girder with Very Thin Metal Web. Zeitchrift Flugtech Motorluf-Schiffahrt, 1929. 20.
5. Miller, R.K., Hedgepeth, J. M., An algorithm for Finite Element Analysis of Partly Wrinkled Membranes. AIAA Journal, 1982. 20(12): p. 1761-1763.
6. Adler, A.L., Mikulas, N. M. Application of A Wrinkled Membrane Finite Element Approach to Advanced Membrane Structures. in 42nd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference. 2001.AIAA 2001-4646.
7. Wong, Y.W., and Pellegrino, S. Computation of Wrinkle Amplitudes in Thin Membranes. in 43rd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference. 2002. Denver, CO.AIAA 2002-1369.
8. Deng, X., and Pellegrino, S. Computation of Partially Inflated Shapes of Stratospheric Ballon Structures. in 49th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference. 2008. Schaumburg, IL.AIAA 2008-2133.
9. Wong, Y.W., and Pellegrino, S., Wrinkled Membranes. Part II: Analytical Models. Journal of Mechanics of Materials and Structures, 2006. 11(1): p. 25-59.
10. Haseganu, E.M., and Steigmann, D. J., Analysis of Partly Wrinkled Membranes by The Method of Dynamic Relaxation. Computational Mechanics, 1994. 14(6): p. 596-614.
11. Kashiwa, M., and Onoda J. Wrinkling Analysis Using Improved Dynamic Relaxation Method. in 48th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference. 2007. Honolulu, Hawaii.AIAA 2007-2350.
12. Hossain, N.M.A., Jenkins, C. H., Woo, K. and Igawa, H., Transverse Vibration Analysis for Partly Wrinkled Membranes. Journal of Spacecraft and Rockets, 2006. 43(3): p. 626-637.
13. Anderson, J.D., Hypersonic and High Temperature Gas Dynamics. 2000, Reston, VA: American Institute of Aeronautics and Astronautics.
14. Kinney, D. Fast Methods for Fluid Structural Interactions. 2009.AIAA-2009-1104.
15. Xu, K., A Gas-Kinetic BGK Scheme for the Navier-Stokes Equations and Its Connection with Artificial Dissipation and Godunov Method. Journal of Computational Physics, 2001. 171: p. 289.
16. Xu, K., and Mao, M., A Multidimensional Gaskinetic BGK Scheme for Hypersonic Viscous Flow. Journal of Computational Physics, 2005. 203: p. 405-421.
17. Jenkins, C.H., Haugen, F., and Spicher, W. H., Experimental Measurement of Wrinkling in Membranes Undergoing Planar Deformation. Experimental Mechanics, 1998. 38(2): p. 147-152.
18. Buck, G.M. Testing of Flexible Ballutes in Hypersonic Wind Tunnel for Planetary Aerocapture. in 44th AIAA Aerospace Science Meeting and Exibit. 2006. Reno, NV.AIAA 2006-1319.