Online Books by
William L. Ko
Books from the extended shelves:
- Ko, William L.: Combined compressive and shear buckling analysis of hypersonic aircraft structural sandwich panels (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1991), also by Raymond H. Jackson and Dryden Flight Research Facility (page images at HathiTrust)
- Ko, William L.: Combined-load buckling behavior of metal-matrix composite sandwich panels under different thermal environments (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1991), also by Raymond H. Jackson and Dryden Flight Research Facility (page images at HathiTrust)
- Ko, William L.: Compressive buckling analysis of hat-stiffened panel (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ;, 1991), also by Raymond H. Jackson and Dryden Flight Research Facility (page images at HathiTrust)
- Ko, William L.: Delamination stresses in semicircular laminated composite bars (National Aeronautics and Space Administration, Scientific and Technical Information Division, 1988), also by United States. National Aeronautics and Space Administration. Scientific and Technical Information Division (page images at HathiTrust)
- Ko, William L.: Elastic constants for superplastically formed/diffusion bonded corrugated sandwich core (National Aeronautics and Space Administration, 1980), also by E. S. Harrison, Hugh L. Dryden Flight Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
- Ko, William L.: Finite-element reentry heat-transfer analysis of space shuttle orbiter (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1986), also by Leslie Gong, Robert D. Quinn, and Ames Research Center (page images at HathiTrust)
- Ko, William L.: Multilayer theory for delamination analysis of a composite curved bar subjected to end forces and end moments (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1989), also by Raymond H. Jackson and Dryden Flight Research Facility (page images at HathiTrust)
- Ko, William L.: Open-mode delamination stress concentrations in horseshoe and elliptic composite curved bars subjected to end forces (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1990), also by Raymond H. Jackson and Dryden Flight Research Facility (page images at HathiTrust)
- Ko, William L.: Optimum element density studies for finite-element thermal analysis of hypersonic aircraft structures (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1990), also by Kyle M. Muramoto, Timothy Olona, and Dryden Flight Research Facility (page images at HathiTrust)
- Ko, William L.: Practical theories for service life prediction of critical aerospace structural components (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992), also by Raymond H. Jackson, Richard C. Monaghan, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Program (page images at HathiTrust)
See also what's at your library, or elsewhere.
Help with reading books -- Report a bad link -- Suggest a new listing
Home -- Search -- New Listings -- Authors -- Titles -- Subjects -- Serials
Books -- News -- Features -- Archives -- The Inside Story
Edited by John Mark Ockerbloom (onlinebooks@pobox.upenn.edu)
OBP copyrights and licenses.