Research Catalog
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Displaying 1-19 of 19 results
Minimum weight design of a leaf spring tapered in thickness and width for the Hubble Space Telecope-space support equipment [microform] / P.I. Rodriguez.
- Text
- [Washington, DC] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; [Springfield, VA : For sale by the National Technical Information Service], 1990.
- 1990
Effects of delaminations on the damped dynamic characteristics of composite laminates [microform] : mechanics and experiments / D.A. Saravanos and D.A. Hopkins.
- Text
- [Washington, DC] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
- 1995
Correlation of finite element free vibration predictions using random vibration test data [microform] / Jeffrey A. Chambers.
- Text
- [Washington, DC] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1994]
- 1994
Buckling of composite beams [microform] : CDDF final report : project no. 91-20 / P. Thompson.
- Text
- MSFC, Ala. : National Aeronautics and Space Administration, Marshall Space Flight Center ; [Springfield, Va. : National Technical Information Service, distributor, 1994]
- 1994
The role of damage-softened material behavior in the fracture of composites and adhesives [microform] / by T. Ungsuwarungsri and W.G. Knauss.
- Text
- Pasadena, CA : Graduate Aeronautical Laboratories, California Institute of Technology ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1986?]
- 1986
Stress intensity factor in a tapered specimen [microform] / Liu Xue-Hui and F. Erdogan.
- Text
- Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : For sale by the National Technical Information Service, 1985]
- 1985
Methods for the identification of material parameters in distributed models for flexible structures [microform] / H.T. Banks, J.M. Crowley, I.G. Rosen.
- Text
- Hampton, VA : Institute for Computer Applications in Science and Engineering, NASA Langley Research Center ; [Springfield, Va. : For sale by the National Technical Information Service, 1986]
- 1986
Computational methods for optimal linear-quadratic compensators for infinite dimensional discrete-time systems [microform] / J.S. Gibson, I.G. Rosen.
- Text
- Hampton, VA : NASA Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1986]
- 1986
Computational methods for the identification of spatially varying stiffness and damping in beams [microform] / H.T. Banks, I.G. Rosen.
- Text
- Hampton, VA : NASA Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1986]
- 1986
Interlaminar fracture characterization [microform] : a current review / Roderick H. Martin.
- Text
- Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1991]
- 1991
- 1 Resource
Available Online
http://purl.access.gpo.gov/GPO/LPS59868Investigation of fiber bridging in double cantilever beam specimens [microform] / W. S. Johnson and P. D. Mangalgiri.
- Text
- Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1986]
- 1986
An improved finite-difference analysis of uncoupled vibrations of tapered cantilever beams [microform] / K.B. Subrahmanyam and K.R.V. Kaza.
- Text
- [Washington, D.C. : National Aeronautics and Space Administration, 1984]
- 1984
Planar dynamics of a uniform beam with rigid bodies affixed to the ends / by Joel Storch, Stephen Gates.
- Text
- Cambndge, Massachusetts : The Charles Stark Draper Laboratory, Inc. ; Houston, TX : National Aeronautics and Space Administration, Johnson Space Center, 1993.
- 1993
- 1 Resource
Available Online
https://purl.fdlp.gov/GPO/gpo46423Planar dynamics of a uniform beam with rigid bodies affixed to the ends / by Joel Storch, Stephen Gates.
- Text
- Cambndge, Massachusetts : The Charles Stark Draper Laboratory, Inc. ; Houston, TX : National Aeronautics and Space Administration, Johnson Space Center, 1993.
- 1983
The analysis of adhesively bonded advanced composite joints using joint finite elements / Scott E. Stapleton and Anthony M. Waas.
- Text
- Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, April 2012.
- 2012-4
- 1 Resource
Available Online
https://purl.fdlp.gov/GPO/gpo59436Development and application of benchmark examples for mixed-mode I/II quasi-static delamination propagation predictions / Ronald Krueger.
- Text
- Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, April 2012.
- 2012-4
- 1 Resource
Available Online
https://purl.fdlp.gov/GPO/gpo32908Improved displacement transfer functions for structure deformed shape predictions using discretely distributed surface strains / William L. Ko and Van Tran Fleischer.
- Text
- Edwards, CA : National Aeronautics and Space Administration, Dryden Flight Research Center, 2012.
- 2012
- 1 Resource
Available Online
https://purl.fdlp.gov/GPO/gpo37308First- and second-order displacement transfer functions for structural shape calculations using analytically predicted surface strains / William L. Ko and Van Tran Fleischer.
- Text
- Edwards, CA : National Aeronautics and Space Administration, Dryden Flight Research Center, 2012.
- 2012
- 1 Resource
Available Online
https://purl.fdlp.gov/GPO/gpo37309A test for characterizing delamination migration in carbon/epoxy tape laminates / James G. Ratcliffe, Michael W. Czabaj and Thomas K. O'Brien.
- Text
- Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, August 2013.
- 2013-8
- 1 Resource
Available Online
https://purl.fdlp.gov/GPO/gpo54339
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