Active filters
Displaying 16 of 16 results
Three point lead screw positioning apparatus [microform] / inventor, Frank S. Calco.
Text
[Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1992]
1992
0 resources
Equivalent plate analysis of aircraft wing box structures with general planform geometry [microform] / Gary L. Giles.
Text
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1986]
1986
1 resource
Available online
http://purl.access.gpo.gov/GPO/LPS85490The construction of airfoil pressure models by the bonded plate method [microform] : achievements, current research, technology development and potential applications / Pierce L. Lawing.
Text
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1985]
1985
0 resources
Contact stresses in pin-loaded orthotropic plates [microform] / M. W. Hyer, E. C. Klang.
Text
Blacksburg, Va. : College of Engineering, Virginia Polytechnic Institute and State University ; [Hampton, Va. : National Aeronautics and Space Administration, Applied Materials Branch, Langley Research Center, [1984]
1984
1 resource
Available online
http://purl.access.gpo.gov/GPO/LPS87558Surface cracks in a plate of finite width under tension or bending [microform] / F. Erdogan and H. Boduroglu.
Text
Bethlehem, Pa. : Lehigh University ; Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1984]
1984
0 resources
The modeling of piezoceramic patch interactions with shells, plates and beams [microform] / H.T. Banks, R.C. Smith.
Text
Hampton, Va. : National Aeronautics and Space Administration, Institute for Computer Applications in Science and Engineering, Langley Research Center, [1992]
1992
1 resource
Available online
http://purl.access.gpo.gov/GPO/LPS97953A three-node C̊ element for analysis of laminated composite sandwich shells [microform] / C. Wayne Martin, S.F. Lung, and K.K. Gupta.
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, 1989.
1989
1 resource
Available online
http://purl.access.gpo.gov/GPO/LPS96605Observation of the initiation and progression of damage in compressively loaded composite plates containing a cutout [electronic resource] / Anthony Waas and Charles Babcock, Jr.
Text
Pasadena, Calif. : Graduate Aeronautical Laboratories, California Institute of Technology ; [Washington, D.C.? : National Aeronautics and Space Administration, 1986]
1986
1 resource
Available online
http://purl.access.gpo.gov/GPO/LPS112451Observation of the initiation and progression of damage in compressively loaded composite plates containing a cutout [microform] / Anthony Waas and Charles Babcock, Jr.
Text
Pasadena, Calif. : Graduate Aeronautical Laboratories, California Institute of Technology ; [Washington, D.C.? : National Aeronautics and Space Administration, 1986]
1986
1 resource
Available online
http://purl.access.gpo.gov/GPO/LPS112451Experimental assessment of advanced Stirling component concepts [microform] / B. Ziph ; prepared for National Aeronautics and Space Administration, Lewis Research Center for U.S. Department of Energy, Conservation and Renewable Energy, Office of Vehicle and Engine R&D. under interagency agreement DE-A101-77CS51040.
Text
Ann Arbor, MI. : Stirling Thermal Motors, Inc. ; Washington, D.C. : U.S. Dept. of Energy, [1985]
1985
0 resources
Plates and shells containing a surface crack under general loading conditions [microform] / Paul F. Joseph and Fazil Erdogan.
Text
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1987]
1987
0 resources
Cubic zig-zag enrichment of the classical Kirchhoff kinematics for laminated and sandwich plates / Michael P. Nemeth.
Text
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [2012]
2012
1 resource
Available online
https://purl.fdlp.gov/GPO/gpo28057Conditions for symmetries in the buckle patterns of laminated-composite plates / Michael P. Nemeth.
Text
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [2012]
2012
1 resource
Available online
https://purl.fdlp.gov/GPO/gpo30943On hybrid and mixed finite element methods / Th. H.H. Pian.
Text
Cambridge, Massachusetts : Massachusetts Institute of Technology ; [Washington, DC] : National Aeronautics and Space Administration, 1981.
1981
1 resource
Available online
https://purl.fdlp.gov/GPO/gpo46542On hybrid and mixed finite element methods / Th. H.H. Pian.
Text
Cambridge, Massachusetts : Massachusetts Institute of Technology ; [Washington, DC] : National Aeronautics and Space Administration, 1981.
1981
0 resources
Finite element analysis of composite joint configurations with gaps and overlaps / Ronald Krueger.
Text
Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, June 2014.
2014-6
1 resource
Available online
https://purl.fdlp.gov/GPO/gpo54829No results found from Digital Research Books Beta
Digital books for research from multiple sources worldwide - all free to read, download, and keep. No library card required.
Explore Digital Research Books Beta