Accession Number:

AD0917344

Title:

SST Technology Follow-On Program-Phase II. Crack Propagation and Residual Strength Testing of Titanium Structure.

Descriptive Note:

Final rept. on Task 1,

Corporate Author:

BOEING COMMERCIAL AIRPLANE CO SEATTLE WA

Report Date:

1974-01-01

Pagination or Media Count:

167.0

Abstract:

This report presents the results of crack growth and residual strength tests from the SST program. These results are summarized into parametric charts and compared with published analytical methods. Author

Subject Categories:

  • Transport Aircraft
  • Metallurgy and Metallography
  • Mechanics

Distribution Statement:

APPROVED FOR PUBLIC RELEASE