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.
Handbook of analytical methods for textile composites under contract NAS1-19243 /Format: [microform] :
Author: Cox, Brian N.
Publisher: Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ;
Date: 1997] This title can be found in 2 Iowa libraries.
Fatigue life methodology for tapered composite flexbeam laminatesFormat: [microform] /
Author: Murri, Gretchen B.
Publisher: [Washington, DC : National Aeronautics and Space Administration ;
Date: 1997] This title can be found in 2 Iowa libraries.
Tracer lamination in the stratosphere a global climatology /Format: [microform] :
Author: Appenzeller, Christof.
Publisher: [Washington, DC : National Aeronautics and Space Administration ;
Date: 1997] This title can be found in 2 Iowa libraries.
A higher-order bending theory for laminated composite and sandwich beamsFormat: [microform] /
Author: Cook, Geoffrey M.
Publisher: Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ;
Date: 1997] This title can be found in 2 Iowa libraries.
Fatigue life methodology for tapered composite flexbeam laminatesFormat: [microform] /
Author: Murri, Gretchen B.
Publisher: Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ;
Date: 1997] This title can be found in 2 Iowa libraries.
Analysis of smart composite structures including debondingFormat: [microform] /
Author: Chattopadhyay, Aditi.
Publisher: [Washington, DC : National Aeronautics and Space Administration ;
Date: 1997] This title can be found in 2 Iowa libraries.
The impact response of carbon/epoxy laminatesFormat: [microform] /
Author: Nettles, A. T.
Publisher: [Huntsville, Ala.] : National Aeronautics and Space Administration, Marshall Space Flight Center ;
Date: [1997] This title can be found in 1 Iowa libraries.
Layerwise finite elements for smart piezoceramic composite plates in thermal environmentsFormat: [microform] /
Author: Lee, Ho-Jun.
Publisher: [Washington, DC] : National Aeronautics and Space Administration ;
Date: 1996] This title can be found in 2 Iowa libraries.
Buckling and postbuckling behavior of laminated composite plates with a cutoutFormat: [microform] /
Author: Nemeth, Michael P.
Publisher: Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ;
Date: 1996] This title can be found in 2 Iowa libraries.
The influence of lamination angles on the interior noise levels of an aircraftFormat: [microform] /
Author: Fernholz, Christian M.
Publisher: Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ;
Date: 1996] This title can be found in 2 Iowa libraries.
Progressive Damage Analysis of Laminated Composite (PDALC)--a computational model implemented in the NASA COMET finite element codeFormat: [microform] /
Publisher: Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ;
Date: 1996] This title can be found in 2 Iowa libraries.
Prediction of composite laminate fracture micromechanics and progressive fracture /Format: [microform] :
Author: Gotsis, Pascal K.
Publisher: [Washington, D.C. : National Aeronautics and Space Administration ;
Date: 1996] This title can be found in 2 Iowa libraries.
Coupled mixed-field laminate theory and finite element for smart piezolectric composite shell structuresFormat: [microform] /
Author: Saravanos, D. A.
Publisher: [Washington, D.C.] : National Aeronautics and Space Administration ;
Date: 1996] This title can be found in 2 Iowa libraries.
Endoscopic shearography and thermography methods for nondestructive evaluation of lined pressure vessels (5-33977) final technical report for period 1 October 1995 through 29 September 1996 : technical report 5-33977, contract no. NAS8-38609, delivery order no. 152 /Format: [microform] :
Author: Lansing, Matthew D.
Publisher: [Washington, DC : National Aeronautics and Space Administration ;
Date: 1996] This title can be found in 2 Iowa libraries.
Analysis of the progressive failure of brittle matrix compositesFormat: [microform] /
Author: Thomas, David J.
Publisher: [Springfield, Va. : National Technical Information Service, distributor, [Springfield, Va. : National Technical Information Service, distributor,
Date: 1995] This title can be found in 2 Iowa libraries.
Effects of delaminations on the damped dynamic characteristics of composite laminates mechanics and experiments /Format: [microform] :
Author: Saravanos, D. A.
Publisher: [Springfield, Va. : National Technical Information Service, distributor, [Springfield, Va. : National Technical Information Service, distributor,
Date: 1995] This title can be found in 2 Iowa libraries.
Probabilistic fiber composite micromechanicsFormat: [microform] /
Author: Stock, Thomas A.
Publisher: Cleveland, Ohio : Cleveland State University ;
Date: 1995] This title can be found in 2 Iowa libraries.
Composite processing development to improve interlaminar strength using ply interface particles (Center Director's discretionary fund final report, no. 93-13) /Format: [microform] :
Author: Nettles, A. T.
Publisher: MSFC, Ala. : National Aeronautics and Space Administration, George C. Marshall Space Flight Center ;
Date: 1995] This title can be found in 2 Iowa libraries.
Development of a composite tailoring procedure for airplane wing progress reportFormat: [microform] /
Author: Chattopadhyay, Aditi.
Publisher: [Washington, DC : National Aeronautics and Space Administration ;
Date: 1995] 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.