Книги з теми "Stiffened composite panel"
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L, Phillips John. Structural analysis and optimum design of geodesically stiffened composite panels. Blacksburg, Va: Virginia Polytechnic Institute and State University, Center for Composite Materials and Structures, 1990.
Знайти повний текст джерелаSimitses, George J. Buckling of delaminated long panels under pressure and of radially-loaded stiffened annular plates. Atlanta, Ga: Georgia Institute of Technology, 1985.
Знайти повний текст джерелаLevon, Minnetyan, and United States. National Aeronautics and Space Administration., eds. Discontinuously stiffened composite panel under compressive loading. [Washington, DC: National Aeronautics and Space Administration, 1995.
Знайти повний текст джерелаDetailed analysis and test correlation of a stiffened composite wing panel. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1991.
Знайти повний текст джерелаW, Hyer M., and United States. National Aeronautics and Space Administration., eds. Calculation of skin-stiffener interface stresses in stiffened composite panels. Blacksburg, Virginia: College of Engineering, Virginia Polytechnic Institute and State University, 1987.
Знайти повний текст джерелаW, Hyer M., and United States. National Aeronautics and Space Administration, eds. Calculation of skin-stiffener interface stresses in stiffened composite panels. Blacksburg, Virginia: College of Engineering, Virginia Polytechnic Institute and State University, 1987.
Знайти повний текст джерелаW, Hyer M., and United States. National Aeronautics and Space Administration, eds. Calculation of skin-stiffener interface stresses in stiffened composite panels. Blacksburg, Virginia: College of Engineering, Virginia Polytechnic Institute and State University, 1987.
Знайти повний текст джерелаCalculation of skin-stiffener interface stresses in stiffened composite panels. Blacksburg, Virginia: College of Engineering, Virginia Polytechnic Institute and State University, 1987.
Знайти повний текст джерелаCalculation of skin-stiffener interface stresses in stiffened composite panels. Blacksburg, Virginia: College of Engineering, Virginia Polytechnic Institute and State University, 1987.
Знайти повний текст джерелаStructural analysis and design of geodesically stiffened composte panels with variable stiffener distribution. [Washington, DC: National Aeronautics and Space Administration, 1992.
Знайти повний текст джерелаFormulation of an improved smeared stiffener theory for buckling analysis of grid-stiffened composite panels. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1995.
Знайти повний текст джерелаR, Ambur Damodar, and United States. National Aeronautics and Space Administration., eds. Response of composite panels with stiffness gradients due to stiffener terminations and cutouts. [Washington, D.C: National Aeronautics and Space Administration, 1997.
Знайти повний текст джерелаUnited States. National Aeronautics and Space Administration. Scientific and Technical Information Branch., ed. Abrasion behavior of aluminum and composite skin coupons, stiffened skins, and stiffened panels representative of transport airplane structures. [Washington, D.C.]: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1985.
Знайти повний текст джерелаFatigue Response of Thin Stiffened Alumminum Cracked Panels Repaired with Bonded Composite Patches. Storming Media, 2001.
Знайти повний текст джерелаR, Ambur Damodar, and United States. National Aeronautics and Space Administration., eds. Response of composite panels with stiffness gradients due to stiffener terminations and cutouts. [Washington, D.C: National Aeronautics and Space Administration, 1997.
Знайти повний текст джерелаImprovements to a method for the geometrically nonlinear analysis of compressively loaded stiffened composite panels: Final technical report February 1991-December 1993. [Washington, DC: National Aeronautics and Space Administration, 1993.
Знайти повний текст джерелаUnited States. National Aeronautics and Space Administration., ed. Improvements to a method for the geometrically nonlinear analysis of compressively loaded stiffened composite panels: Progress report for the period July 1991 to December 1991. [Washington, DC: National Aeronautics and Space Administration, 1991.
Знайти повний текст джерелаTwo-dimensional sequential and concurrent finite element analysis of unstiffened and stiffened aluminum and composite panels with hole. Norfolk, Va: Department of Civil Engineering, College of Engineering and Technology, Old Dominion University, 1988.
Знайти повний текст джерелаVenkatesh, Prasad, and United States. National Aeronautics and Space Administration., eds. Two-dimensional sequential and concurrent finite element analysis of unstiffened and stiffened aluminum and composite panels with hole. Norfolk, Va: Department of Civil Engineering, College of Engineering and Technology, Old Dominion University, 1988.
Знайти повний текст джерелаNational Aeronautics and Space Administration (NASA) Staff. Two-Dimensional Sequential and Concurrent Finite Element Analysis of Unstiffened and Stiffened Aluminum and Composite Panels with Hole. Independently Published, 2018.
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