Thermostructural analysis of unconventional wing structures of a Hyper-X hypersonic flight research vehicle for the Mach 7 missionFormat: [microform] /
Author: Ko, William L.
Publisher: Edwards, Calif. : National Aeronautics and Space Administration, Dryden Flight Research Center ;
Date: [2001] This title can be found in 1 Iowa libraries.
Open-mode debonding analysis of curved sandwich panels subjected to heating and cryogenic cooling on opposite facesFormat: [microform] /
Author: Ko, William L.
Publisher: Edwards, Calif. : National Aeronautics and Space Administration, Dryden Flight Research Center ;
Date: 1999] This title can be found in 2 Iowa libraries.
Mechanical- and thermal-buckling behavior of rectangular plates with different central cutoutsFormat: [microform] /
Author: Ko, William L.
Publisher: Edwards, Calif. : Dryden Flight Research Center, National Aeronautics and Space Administration ;
Date: [1998] This title can be found in 1 Iowa libraries.
Anomalous buckling characteristics of laminated metal-matrix composite plates with central square holesFormat: [microform] /
Author: Ko, William L.
Publisher: Edwards, Calif. : National Aeronautics and Space Administration, Dryden Flight Research Center ;
Date: [1998] This title can be found in 2 Iowa libraries.
Stress analysis of B-52 pylon hooks for carrying the X-38 drop test vehicleFormat: [microform] /
Author: Ko, William L.
Publisher: Edwards, Calif. : National Aeronautics and Space Administration, Dryden Flight Research Center ;
Date: 1997] This title can be found in 2 Iowa libraries.
Thermostructural behavior of a hypersonic aircraft sandwich panel subjected to heating on one sideFormat: [microform] /
Author: Ko, William L.
Publisher: [Washington, D.C.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ;
Date: 1997. This title can be found in 2 Iowa libraries.
Thermal and mechanical buckling analysis of hypersonic aircraft hat-stiffened panels with varying face sheet geometry and fiber orientationFormat: [microform] /
Author: Ko, William L.
Publisher: [Washington, DC] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ;
Date: 1996. This title can be found in 2 Iowa libraries.
Predictions of thermal buckling strengths of hypersonic aircraft sandwich panels using minimum potential energy and finite element methodsFormat: [microform] /
Author: Ko, William L.
Publisher: [Washington, D.C.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ;
Date: 1995] This title can be found in 1 Iowa libraries.
Mechanical and thermal buckling analysisi of rectangular sandwich panels under different edge conditionsFormat: [microform] /
Author: Ko, William L.
Publisher: [Washington, DC] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ;
Date: 1994. This title can be found in 1 Iowa libraries.
Thermocryogenic buckling and stress analyses of a partially filled cryogenic tank subjected to cylindrical strip heatingFormat: [microform] /
Author: Ko, William L.
Publisher: [Washington, DC] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ;
Date: 1994. This title can be found in 2 Iowa libraries.
Shear buckling analysis of a hat-stiffened panelFormat: [microform] /
Author: Ko, William L.
Publisher: [Washington, DC] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ;
Date: 1994. This title can be found in 2 Iowa libraries.
Mechanical and thermal buckling analysis of sandwich panels under different edge conditionsFormat: [microform] /
Author: Ko, William L.
Publisher: [Springfield, Va. : National Technical Information Service, distributor], [Springfield, Va. : National Technical Information Service, distributor],
Date: 1993. This title can be found in 2 Iowa libraries.
Compressive and shear buckling analysis of metal matrix composite sandwich panels under different thermal environmentsFormat: [microform] /
Author: Ko, William L.
Publisher: [Washington, DC] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ;
Date: 1993. This title can be found in 1 Iowa libraries.
Practical theories for service life prediction of critical aerospace structural components /Author: Ko, William L.
Publisher: [Washington, DC] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program,
Date: 1992. This title can be found in 1 Iowa libraries.
Combined compressive and shear buckling analysis of hypersonic aircraft structural sandwich panels /Author: Ko, William L.
Publisher: [Washington, DC] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division,
Date: 1991. This title can be found in 1 Iowa libraries.
Combined-load buckling behavior of metal-matrix composite sandwich panels under different thermal environments /Author: Ko, William L.
Publisher: [Washington, DC] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program,
Date: 1991. This title can be found in 1 Iowa libraries.
Compressive buckling analysis of hat-stiffened panel /Author: Ko, William L.
Publisher: [Washington, DC] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program,
Date: 1991. This title can be found in 1 Iowa libraries.
Application of fracture mechanics and half-cycle method to the prediction of fatigue life of B-52 aircraft pylon components /Publisher: Edwards, Calif. : National Aeronautics and Space Administration, Ames Research Center, Dryden Flight Research Facility,
Date: 1989. This title can be found in 1 Iowa libraries.
Open-mode delamination stress concentrations in horseshoe and elliptic composite curved bars subjected to end forces /Author: Ko, William L.
Publisher: [Washington, DC] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division,
Date: 1990. This title can be found in 1 Iowa libraries.
Optimum element density studies for finite-element thermal analysis of hypersonic aircraft structures /Author: Ko, William L.
Publisher: [Washington, DC] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division,
Date: 1990. This title can be found in 1 Iowa libraries.
This resource is supported by the Institute of Museum and Library Services under the provisions of the Library Services and Technology Act as administered by State Library of Iowa.