Elastic plates and shells -- Vibration -- Mathematical models
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Applications of the theory of optimal control of distributed-parameter systems to structural optimization (National Aeronautics and Space Administration ;, 1972), by Jean-Louis Pierre Armand, Langley Research Center, and Stanford University (page images at HathiTrust)
- Free vibrations of thermally stressed orthotropic plates with various boundary conditions (National Aeronautics and Space Administration ;, 1973), by C. D. Bailey, James C. Greetham, Langley Research Center, and Ohio State University. Research Foundation (page images at HathiTrust)
- Effects of structural damping on flutter of stressed panels (National Aeronautics and Space Administration ;, 1969), by Charles P. Shore, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
- Small oscillations of thin resilient conical shells (National Aeronautics and Space Administration, 1960), by Ėduard Ivanovich Grigoli︠u︡k (page images at HathiTrust)
- Axisymmetric oscillation of a partially liquid-filled cylindrical shell container having hemispherical bulkheads (National Aeronautics and Space Administration ;, 1973), by Rudolf F. Glaser and George C. Marshall Space Flight Center (page images at HathiTrust)
Items below (if any) are from related and broader terms.
Filed under: Elastic plates and shells -- Vibration- Vibration of a floating ice sheet (Corps of Engineers, U.S. Army Cold Regions Research and Engineering Laboratory, 1970), by D. E Nevel (page images at HathiTrust)
- NASA TN D-5759 (National Aeronautics and Space Administration :, 1970), by Sidney C. Dixon, M. Latrelle Hudson, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
- NASA TN D-4221 (National Aeronautics and Space Administration ;, 1967), by Vasant S. Kelkar, Ames Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
- Lamb waves at ultrasonic frequencies (U.S. Atomic Energy Commission, 1959), by D. C. Worlton, United States. National Bureau of Standards, United States. Department of Energy. Office of Fusion Energy, United States. National Bureau of Standards. Fracture and Deformation Division, U.S. Atomic Energy Commission, United States. Energy Research and Development Administration, Hanford Works, and Hanford Atomic Products Operation. Engineering Operation (page images at HathiTrust)
- Experimenmtal flutter results for corrugation-stiffened and unstiffened panels (National Aeronautics and Space Administration ;, 1966), by Deene J. Weidman and Langley Research Center (page images at HathiTrust)
- NASA TN D-3030 (National Aeronautics and Space Administration ; [For sale by the Office of Technical Services, Department of Commerce, Washington, D.C. 20230], 1965), by Robert E. Reed, Ames Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
- Vibration testing of impact-damaged composite laminates (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1989), by Joseph H. Grady and Erwin H. Meyn (page images at HathiTrust)
- NASA TN D-6090 (National Aeronautics and Space Administration :, 1971), by James A. Schoenster, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
- Vibration of shells (Scientific and Technical Information Office, National Aeronautics and Space Administration; [for sale by the Supt. of Docs., U.S. Govt. Print. Off.], 1973), by Arthur W. Leissa (page images at HathiTrust)
- Diffracted and head waves associated with waves on nonseparable surfaces (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992), by Raymond L. Barger and Langley Research Center (page images at HathiTrust)
- Flexural vibrations of conical shells with free edges (National Aeronautics and Space Administration, 1966), by W. C. L. Hu, U. S. Lindholm, and J. F. Gormley (page images at HathiTrust; US access only)
- On the differential equations of the axisymmetric vibration of paraboloidal shells of revolution (National Aeronautics and Space Administration, 1967), by James Ting-shun Wang and Chi-wen Lin (page images at HathiTrust; US access only)
- NASA TN D-6473 (National Aeronautics and Space Administration ;, 1971), by Eugene C. Naumann, William C. Walton, Donnell S. Catherines, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
- NASA TN D-6089 (National Aeronautics and Space Administration :, 1971), by John L. Sewall, Christine G. Pusey, William M. Thompson, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
- A method for computation of vibration modes and frequencies of orthotropic thin shells of revolution having general meridional curvature (National Aeronautics and Space Administration, 1969), by Howard M. Adelman, William C. Walton, Donnell S. Catherines, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
- NASA TN D-4221 (National Aeronautics and Space Administration ;, 1967), by Vasant S. Kelkar, Ames Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
- NASA TN D-2666 (National Aeronautics and Space Administration :, 1965), by William C. L. Hu and United States National Aeronautics and Space Administration (page images at HathiTrust)
- A study of the vibrations of shallow spherical shells (Aberdeen Proving Ground, Maryland : Ballistic Research Labortories, 1963., 1963), by W. H. Hoppmann, C. N. Baronet, and U.S. Army Ballistic Research Laboratory (page images at HathiTrust)
- NASA TN D-4090 (National Aeronautics and Space Administration ;, 1967), by David A. Evensen, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
- Conical shell vibrations (National Aeronautics and Space Administration ;, 1965), by Daniel H. Platus and inc ARA (page images at HathiTrust)
- NASA TN D-6473 (National Aeronautics and Space Administration ;, 1971), by Eugene C. Naumann, William C. Walton, Donnell S. Catherines, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
- NASA TN D-6106 (National Aeronautics and Space Administration :, 1971), by Robert Miserentino, Sidney C. Dixon, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
- NASA TN D-5663 (National Aeronautics and Space Administration ; [For sale for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1970), by John L. Sewall, Donnell S. Catherines, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
- NASA TN D-6557 (National Aeronautics and Space Administration ; [For sale for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1971), by Eugene C. Naumann, John S. Mixson, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
- Modal interaction in postbuckled plates : theory (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1989), by Gaylen A. Thurston and Langley Research Center (page images at HathiTrust)
- Application of Newton's method to postbuckling of rings under pressure loadings (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1989), by Gaylen A. Thurston and Langley Research Center (page images at HathiTrust)
- A three-node C ̊element for analysis of laminated composite sandwich shells (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1989), by C. Wayne Martin, K. K. Gupta, and S. F. Lung (page images at HathiTrust)
- Theoretical study of corrugated plates : shearing of a trapezoidally corrugated plate with through lines permitted to curve (National Aeronautics and Space Administration, 1971), by Chuan-jui Lin, Charles Libove, United States. National Aeronautical and Space Administration, Syracuse University, and Langley Research Center (page images at HathiTrust)
- Buckling analysis for axially compressed flat plates, structural sections, and stiffened plates reinforced with laminated composites (National Aeronautics and Space Administration ;, 1971), by A. V. Viswanathan, R. E. Miller, Tsai-Chen Soong, Langley Research Center, and Boeing Company (page images at HathiTrust)
- Elastic stability of laminated, flat and curved, long rectangular plates subjected to combined inplane loads (National Aeronautics and Space Administration ;, 1974), by A. V. Viswanathan, L. L. Baker, M. Tamekuni, Langley Research Center, and Boeing Commercial Airplane Company (page images at HathiTrust)
- Shearing of a corrugated plate with curvilinear corrugations (National Aeronautics and Space Administration ;, 1972), by Lung-Hsiang Wu, Charles Libove, Langley Research Center, and Syracuse University (page images at HathiTrust)
- Elastic buckling analysis for composite stiffened panels and other structures subjected to biaxial inplane loads (National Aeronautics and Space Administration ;, 1973), by A. V. Viswanathan, M. Tamekuni, Langley Research Center, and Boeing Commercial Airplane Company (page images at HathiTrust)
- New triangular and quadrilateral plate-bending finite elements (National Aeronautics and Space Administration ;, 1974), by R. Narayanaswami and Langley Research Center (page images at HathiTrust)
- Multi-ring plates : a Step function approach ([Washington, D.C.] : [United States Air Force, Office of Scientific Research], [1958], 1958), by Patrick M. Quinlan, United States. Air Force. Office of Scientific Research, and National University of Ireland (page images at HathiTrust)
- Mixed formulation for frictionless contact problems (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1989), by Ahmed Khairy Noor and Kyun O. Kim (page images at HathiTrust)
- The effect of angle of attack on the buckling of Mars entry aeroshells (National Aeronautics and Space Administration ;, 1973), by Gerald A. Cohen, Langley Research Center, and Structures Research Associates (page images at HathiTrust)
- Stress analysis of reinforced circular and rectangular flat plates (Argonne National Laboratory, 1965), by J. L. S. Chen, Donald A. Moen, Chia-shing Lai, U.S. Atomic Energy Commission, and Argonne National Laboratory (page images at HathiTrust)
- Buckling behavior of long symmetrically laminated plates subjected to combined loadings (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992), by Michael P. Nemeth and Langley Research Center (page images at HathiTrust)
- Compressive buckling analysis of hat-stiffened panel (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ;, 1991), by William L. Ko, Raymond H. Jackson, and Dryden Flight Research Facility (page images at HathiTrust)
- A solution procedure for behavior of thick plates on a nonlinear foundation and postbuckling behavior of long plates (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1983), by Manuel Stein, Peter A. Stein, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
- Dissociative relaxation of oxygen over an adiabatic flat plate at hypersonic Mach numbers (National Aeronautics and Space Administration, 1960), by Paul M. Chung, Aemer D. Anderson, and Ames Research Center (page images at HathiTrust)
- BAFL-1 : a program for the solution of thin elastic plate equations on the PHILCO-2000 computer (Washington, D.C. : Office of Technical Services, Department of Commerce, 1961., 1961), by J. B. Callaghan, A. K. Rigler, P. H. Jarvis, Westinghouse Electric Corporation, U.S. Atomic Energy Commission, and Bettis Atomic Power Laboratory (page images at HathiTrust)
- Preliminary design of wings. Volume III, Minimum weight design of stiffened plate (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, 1974., 1974), by Harold Switzky, Air Force Flight Dynamics Laboratory (U.S.), and Fairchild Republic Company (page images at HathiTrust)
- Preliminary design of wings. Volume IV, Minimum weight design of composite structure (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, 1974., 1974), by Harold Switzky, Air Force Flight Dynamics Laboratory (U.S.), and Fairchild Republic Company (page images at HathiTrust)
- A triangular thin shell finite element : linear analysis (National Aeronautics and Space Administration ;, 1975), by G. R. Thomas, Richard H. Gallagher, Langley Research Center, and Cornell University (page images at HathiTrust)
- A triangular thin shell finite element : nonlinear analysis (National Aeronautics and Space Administration ;, 1975), by G. R. Thomas, Richard H. Gallagher, Langley Research Center, and Cornell University (page images at HathiTrust)
- Deformations and stresses in circular cylindrical shells caused by pipe attachment. Part VII, Work charts for off-center loading (Schenectady, New York : Knolls Atomic Power Laboratory, 1953., 1953), by M. T. Roche, Knolls Atomic Power Laboratory, General Electric Company, and U.S. Atomic Energy Commission (page images at HathiTrust)
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