Nonlinear structural reduced order modeling methods for hypersonic structures

A. Matney, R. A. Perez, S. M. Spottswood, X. Q. Wang, Marc Mignolet

Research output: Chapter in Book/Report/Conference proceedingConference contribution

6 Citations (Scopus)

Abstract

This paper focuses on the extension and continued validation of coupled thermal-structural reduced order models for the prediction of the nonlinear geometric response of heated panels of hypersonic aircraft. The large spatial and temporal variations of temperature expected in such structures imply similar variations of the material properties, most notably elastic properties and coefficient of thermal expansion, which must be captured for an accurate response prediction. Accordingly, earlier reduced order models are first extended to include linear variations with local temperature of the elasticity tensor and coefficients of thermal expansion. The validation of these concepts is achieved on a beam structural model. A representative 3-D hypersonic panel is considered next in isothermal conditions to extend the validation of nonlinear reduced order modeling methods to complex structural models. Key in the reduced order model construction is the basis selection and the combination of linear and dual modes introduced and validated in prior efforts is once again found to capture well the structural response, although an additional set of functions, referred to as the tangent duals is introduced to complete the structural response modeling. The corresponding predictions of the forced static and dynamic responses are found to match full Nastran results very well.

Original languageEnglish (US)
Title of host publication53rd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference 2012
StatePublished - 2012
Event53rd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference 2012 - Honolulu, HI, United States
Duration: Apr 23 2012Apr 26 2012

Other

Other53rd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference 2012
CountryUnited States
CityHonolulu, HI
Period4/23/124/26/12

Fingerprint

hypersonics
Hypersonic aerodynamics
Thermal expansion
thermal expansion
hypersonic aircraft
beams (supports)
elastic properties
predictions
Hypersonic vehicles
coefficients
dynamic response
tangents
Tensors
Dynamic response
Elasticity
Materials properties
tensors
Temperature
temperature

ASJC Scopus subject areas

  • Aerospace Engineering
  • Mechanical Engineering
  • Materials Science(all)
  • Surfaces and Interfaces

Cite this

Matney, A., Perez, R. A., Spottswood, S. M., Wang, X. Q., & Mignolet, M. (2012). Nonlinear structural reduced order modeling methods for hypersonic structures. In 53rd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference 2012

Nonlinear structural reduced order modeling methods for hypersonic structures. / Matney, A.; Perez, R. A.; Spottswood, S. M.; Wang, X. Q.; Mignolet, Marc.

53rd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference 2012. 2012.

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Matney, A, Perez, RA, Spottswood, SM, Wang, XQ & Mignolet, M 2012, Nonlinear structural reduced order modeling methods for hypersonic structures. in 53rd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference 2012. 53rd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference 2012, Honolulu, HI, United States, 4/23/12.
Matney A, Perez RA, Spottswood SM, Wang XQ, Mignolet M. Nonlinear structural reduced order modeling methods for hypersonic structures. In 53rd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference 2012. 2012
Matney, A. ; Perez, R. A. ; Spottswood, S. M. ; Wang, X. Q. ; Mignolet, Marc. / Nonlinear structural reduced order modeling methods for hypersonic structures. 53rd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference 2012. 2012.
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