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Analytical wing weight prediction/estimation using computer based design techniques

By N. A. D. Murphy
Publisher: Cranfield University
Year: 1987
OAI identifier: oai:dspace.lib.cranfield.ac.uk:1826/3379
Provided by: Cranfield CERES

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Citations

  1. (1974). WAATS -A computer program for weights analysis of advanced transportation systems,
  2. Application of the finite element technique to aerodynamic problems of aircraft, doi
  3. (1970). Application of computer aided design programs for the technical management of complex f ighter development projects. doi
  4. (1979). Hutton et al, Application of finite element analysis to derivation of structural weight,
  5. Khot et al, optimization of fiber reinforced composite structures, doi
  6. (1972). Ladner et al, A summary of the design synthesis process,
  7. (1071). Application of fully stresses design procedures to wing and empennage structures. doi
  8. (1976). A new role for structures technology in aircraft configuration development,
  9. (1960). Rib Weight estimation by structural analysis,
  10. (1969). The derivation and application of analytical -statistical weight prediction techniques,
  11. (1969). optimization of structures to satisfy flutter requirements, doi
  12. Including Your Own Module A104
  13. (B) to (H) These portions of the flow chart are self explanatory and need no further explanation except to say that they are fail-safe mechanisms to prevent accidental deletion of existing databases.

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