Thermal buckling of metal foam sandwich panels for actively cooled thermal protection systems

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

Volumn 3, Issue , 2004, Pages 2206-2221

  Rakow, Joseph F ^a   Waas, Anthony M ^a  

^a UNIVERSITY OF MICHIGAN   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

BUCKLING; FOAMED PRODUCTS; STRAIN GAGES; STRUCTURAL ANALYSIS; STRUCTURAL PANELS; THERMAL INSULATION; THERMOANALYSIS; THERMOMECHANICAL TREATMENT;

SANDWICH PANELS; THERMAL BUCKLING; THERMAL LOADING; THERMAL PROTECTION SYSTEMS;

SANDWICH STRUCTURES;

EID: 16244389317     PISSN: 02734508     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2004-1710     Document Type: Conference Paper

References (19)

1. S.J. Scotti. Thermal protection systems for reusable launch vehicles. Symposium on Structures for Hypersonic Vehicles, ASME International Congress, November 2003.
2. H.N. Kelly and M.L. Blosser. Active cooling from the sixties to NASP. Current Technology for Thermal Protection Systems, NASA CP-3157:189-249, 1992.
3. D.A. Ellis, L.L. Pagel, and D.M. Schaeffer. Design and fabrication of a radiative actively cooled honeycomb sandwich structural panel for hypersonic aircraft. NASA CR-2957, 1978.
4. J.F. Rakow and A.M. Waas. Size effects and the shear response of aluminum foam. Mechanics of Materials, 2004. Available at www.sciencedirect.com under "Articles in Press".
5. J.F. Rakow and A.M. Waas. Size effects in metal foam cores for sandwich structures. AIAA Journal, May 2004.
6. J.F. Rakow and A.M. Waas. The effective isotropic moduli of random fibrous composites, platelet composites, and foamed solids. Mechanics of Advanced Materials and Structures, 11(2):151-173, 2004.
7. F.P. Incropera and D.P. DeWitt. Fundamentals of Heat and Mass Transfer. John Wiley and Sons, New York, NY, fifth edition, 2002.
8. W.L. Ko. Mechanical and thermal buckling analysis of sandwich panels under different edge conditions. NASA TM-4535, 1993.
9. W.L. Ko. Predictions of thermal buckling strengths of hypersonic aircraft sandwich panels using minimum potential energy and finite element methods. NASA TM-4643, May 1995.
10. A.K. Noor and J.M. Peters. Postbuckling of multilayered composite plates subjected to combined axial and thermal loads. In E.A. Thornton, editor, Thermal Structures and Materials for High-Speed Flight, volume 140, pages 183-203, 1992.
11. T. Hause, L. Librescu, and T.F. Johnson. Non-linear response of geometrically imperfect sandwich curved panels under thermomechanical loading. International Journal of Non-Linear Mechanics, 33(6): 1039-1059, 1998.
12. R. Javaheri and M.R. Eslami. Thermal buckling of functionally graded plates based on higher order theory. Journal of Thermal Stresses, 25:603-625, 2002.
13. H.S. Shen. Thermomechanical post-buckling analysis of imperfect laminated plates using a higher-order shear-deformation theory. Computers and Structures, 66(4):395-409, 1998.
14. M.L. Blosser. Boundary conditions for aerospace thermal-structural tests. Progress in Aeronautics and Astronautics, 168:119-144, 1995.
15. W.L. Richards and R.C. Thompson. Titanium honeycomb panel testing. NASA TM-4768, 1996.
16. M.F. Ashby et al. Metal Foam: A Design Guide. Butterworth-Heinemann, Boston, MA, 2000.
17. J. Singer et al. Buckling Experiments: Experimental Methods in Buckling of Thin-walled Structures, volume 1. John Wiley and Sons, New York, NY, 2002.
18. P.S. Theocaris. Moire Fringes in Strain Analysis. Pergamon Press, New York, NY, 1969.
19. J.N. Reddy. Mechanics of Laminated Composite Plates. CRC Press, New York, NY, 1997.