Reengineering Aircraft Structural Life Prediction Using a Digital Twin

By E. Tuegel, Anthony R. Ingraffea, T. Eason, Michael Spottswood. 2011

980 citations recorded by the source corpus.

Reengineering of the aircraft structural life prediction process to fully exploit advances in very high performance digital computing is proposed. The proposed process utilizes an ultrahigh fidelity model of individual aircraft by tail number, a Digital Twin, to integrate computation of structural deflections and temperatures in response to flight conditions, with resulting local damage and material state evolution. A conceptual model of how the Digital Twin can be used for predicting the life of aircraft structure and assuring its structural integrity is presented. The technical challenges to developing and deploying a Digital Twin are discussed in detail.

Subfields: Civil and Structural Engineering, Mechanics of Materials, Statistics and Probability

View Paper: https://www.semanticscholar.org/paper/3d665a49a63e65b619d53f5c84f0afde81a47994

How researchers see this paper

The researchers whose trusted networks rank it highest, strongest advocate first. Every researcher gets a different order.

In Civil and Structural Engineering

  1. Zhen Hu
  2. Sankaran Mahadevan
  3. Chao Hu
  4. Karen E. Willcox
  5. Michele Dassisti
  6. Robert X. Gao
  7. Byeng Dong Youn
  8. Victor C. Li

In Mechanics of Materials

  1. Sankaran Mahadevan
  2. Zhen Hu
  3. Chao Hu
  4. Karen E. Willcox
  5. Michele Dassisti
  6. Robert X. Gao
  7. Byeng Dong Youn
  8. Victor C. Li

In Statistics and Probability

  1. Sankaran Mahadevan
  2. Zhen Hu
  3. Chao Hu
  4. Andrew Yeh-Ching Nee
  5. Michael G. Kapteyn
  6. Jacob V. R. Pretorius
  7. Marina Dabic
  8. Karen E. Willcox

Citations in the corpus