Structural testing of a stitched/resin film infused graphite-epoxy wing boxFormat: [microform] /
Author: Jegley, Dawn C.
Publisher: Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ;
Date: [2001] This title can be found in 1 Iowa libraries.
A new merit function for evaluating the flaw tolerance of composite laminates. Part II,Format: [microform] /
Author: Mikulas, Martin M.
Publisher: Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ;
Date: 2000] This title can be found in 1 Iowa libraries.
Unlined reusable filament wound composite cryogenic tank testingFormat: [microform] /
Author: Murphy, A. W.
Publisher: [Marshall Space Flight Center, Ala.] : National Aeronautics and Space Administration, Marshall Space Flight Center ;
Date: 1999] This title can be found in 2 Iowa libraries.
Buckling and damage resistance of transversely-loaded composite shellsFormat: [microform] /
Author: Wardle, Brian L.
Publisher: [Washington, DC : National Aeronautics and Space Administration ;
Date: 1998] This title can be found in 2 Iowa libraries.
Experimental spin testing of integrally damped composite plates final report on a research project funded through NASA research grant number NCC3-493 /Format: [microform] :
Author: Kosmatka, J. B.
Publisher: La Jolla, Calif. : Division of Structural Engineering, University of California, San Diego ;
Date: 1998] This title can be found in 2 Iowa libraries.
Thermal output of WK-type strain gauges on various materials at cryogenic and elevated temperaturesFormat: [microform] /
Author: Kowalkowski, Matthew K.
Publisher: Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ;
Date: 1998] This title can be found in 1 Iowa libraries.
Thermographic qualification of graphite/epoxy instrumentation racksFormat: [microform] /
Author: Walker, James L.
Publisher: [Washington, DC : National Aeronautics and Space Administration ;
Date: 1998] This title can be found in 2 Iowa libraries.
Adjusting measured weight loss of aged graphite fabric/PMR-15 compositesFormat: [microform] /
Author: Bowles, Kenneth J.
Publisher: [Cleveland, Ohio] : National Aeronautics and Space Administration, Lewis Research Center ;
Date: [1998] This title can be found in 1 Iowa libraries.
Effect of intercalation in graphite epoxy composites on the shielding of high energy radiation /Publisher: [Washington, D.C.] : [National Aeronautics and Space Administration],
Date: [1997] This title can be found in 1 Iowa libraries.
Compression response of a sandwich fuselage keel panel with and without damageFormat: [microform] /
Author: McGowan David M.
Publisher: Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ;
Date: 1997] This title can be found in 1 Iowa libraries.
Fatigue debonding characterization in composite skin/stringer configurationsFormat: [microform] /
Author: Cvitkovich, Michael K.
Publisher: Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ;
Date: 1997] This title can be found in 1 Iowa libraries.
Effect of intercalation in graphite epoxy composites on the shielding of high energy radiationFormat: [microform] /
Publisher: [Washington, DC] : National Aeronautics and Space Administration ;
Date: 1997] This title can be found in 2 Iowa libraries.
A new merit function for evaluating the flaw tolerance of composite laminates. Part II,Format: [microform] /
Author: Mikulas, Martin M.
Publisher: Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ;
Date: 1997] This title can be found in 2 Iowa libraries.
Response of composite panels with stiffness gradients due to stiffener terminations and cutoutsFormat: [microform] /
Publisher: [Washington, D.C. : National Aeronautics and Space Administration ;
Date: 1997] This title can be found in 2 Iowa libraries.
Buckling behavior of long symmetrically laminated plates subjected to shear and linearly varying axial edge loadsFormat: [microform] /
Author: Nemeth, Michael P.
Publisher: Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ;
Date: 1997] This title can be found in 2 Iowa libraries.
Design guidelines for shielding effectiveness, current carrying capability, and the enhancement of conductivity of composite materials under contract NAS8-39983 /Format: [microform] :
Author: Evans, R. W.
Publisher: Marshall Space Flight Center, Ala. : National Aeronautics and Space Administration, [George C. Marshall Space Flight Center ;
Date: 1997] This title can be found in 2 Iowa libraries.
Test report--fault current through graphite filament reinforced plastic under contract NAS8-39983 /Format: [microform] :
Author: Evans, R. W.
Publisher: Marshall Space Flight Center, Ala. : National Aeronautics and Space Administration, [George C. Marshall Space Flight Center ;
Date: 1997] This title can be found in 2 Iowa libraries.
Structural durability of damaged metallic panel repaired with composite patchesFormat: [microform] /
Author: Minnetyan, Levon.
Publisher: [Washington, D.C. : National Aeronautics and Space Administration ;
Date: 1997] This title can be found in 2 Iowa libraries.
Honeycomb core permeability under mechanical loads under contract NAS1-20013 /Format: [microform] :
Publisher: Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ;
Date: 1997] This title can be found in 2 Iowa libraries.
Evaluation of the Edge Crack Torsion (ECT) test for mode III interlaminar fracture toughness of laminated compositesFormat: [microform] /
Publisher: Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ;
Date: 1996] This title can be found in 2 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.