Cover Image

Design, optimization, and evaluation of A1-2139 compression panel with integral T-stiffeners /

Bibliographic Details
Corporate Author:	Langley Research Center
Other Authors:	Mulani, Sameer B.
Format:	Government Document eBook
Language:	English
Published:	Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [2012]
Series:	NASA technical paper ; 2012-217584.
Subjects:	Design optimization. Finite element method. Photogrammetry. Aluminum alloys. Digital systems. Displacement. Buckling.
Online Access:	https://purl.fdlp.gov/GPO/gpo31180

Similar Items

Design, optimization and evaluation of integrally stiffened Al 7050 panel with curved stiffeners /
Published: (2011)

Design, optimization, and evaluation of integrally-stiffened Al-2139 panel with curved stiffeners /
Published: (2011)

Postbuckling delamination of a stiffened composite panel using finite element methods /
by: Natsiavas, S., et al.
Published: (1987)

Buckling test results and preliminary test and analysis correlation from the 8-foot-diameter orthogrid-stiffened cylinder test article TA02 : test dates: 3-6 February 2009 /
by: Hilburger, Mark W. (Mark William)
Published: (2017)

Thermal and mechanical buckling analysis of hypersonic aircraft hat-stiffened panels with varying face sheet geometry and fiber orientation /
by: Ko, William L.
Published: (1996)

Structure-property correlations in Al-Li alloy integrally stiffened extrusions /
by: Hales, Stephen J.
Published: (2001)

Skin/stiffener interface stresses in composite stiffened panels /
by: Wang, James Ting-Shun
Published: (1984)

Mechanical- and thermal-buckling behavior of rectangular plates with different central cutouts /
by: Ko, William L.
Published: (1998)

Impact and penetration of thin aluminum 2024 flat panels at oblique angles of incidence /
by: Ruggeri, Charles R.
Published: (2015)

Simplified models for the study of postbuckled hat-stiffened composite panels /
by: Vescovini, Riccardo
Published: (2012)

Theoretical and software considerations for nonlinear dynamic analysis /
by: Schmidt, Richard J.
Published: (1983)

Buckling and postbuckling behavior of compression-loaded isotropic plates with cutouts /
by: Nemeth, Michael P.
Published: (1990)

Predictive compensator optimization for head tracking lag in virtual environments /
by: Adelstein, Bernard D., et al.
Published: (2001)

Predictive compensator optimization for head tracking lag in virtual environments /
by: Adelstein, Bernard D.
Published: (2001)

Further development of Ko displacement theory for deformed shape predictions of nonuniform aerospace structures /
by: Ko, William L.
Published: (2009)

Evaluation of pressurization fatigue life of 1441 Al-Li fuselage panel /
by: Bird, R. Keith, et al.
Published: (1999)

Finite and boundary element modeling of the NASA Langley aluminum testbed cylinder (ATC) /
by: Grosveld, Ferdinand W.
Published: (2006)

Probabilistic assessment of National Wind Tunnel /
by: Shah, A. R., et al.
Published: (1996)

Impact testing and simulation of composite airframe structures /
by: Jackson, Karen E.
Published: (2014)

Method for estimating operational loads on aerospace structures using span-wisely distributed surface strains /
by: Ko, William L., et al.
Published: (2013)

Evaluation of Ti-48Al-2Cr-2Nb under fretting conditions /
Published: (2001)

Burst testing of a superalloy disk with a dual grain structure /
by: Gayda, John
Published: (2002)

Burst testing of a superalloy disk with a dual grain structure /
by: Gayda, John, et al.
Published: (2002)

MSFC evaluation of the space fabrication demonstration system (beam builder) /
by: Adams, E. O., et al.
Published: (1981)

A weak Hamiltonian finite element method for optimal control problems /
by: Hodges, Dewey H., et al.
Published: (1989)

Compression response of a sandwich fuselage keel panel with and without damage /
by: McGowan, David M., et al.
Published: (1997)

Modeling progressive damage using local displacement discontinuities within the FEAMAC multiscale modeling framework /
by: Ranatunga, Vipul
Published: (2010)

A new implementation of the Programming System for Structural Synthesis (PROSSS-2) /
by: Rogers, James L.
Published: (1986)

Investigation of methods for selectively reinforcing aluminum and aluminum-lithium materials /
by: Bird, R. Keith
Published: (2013)

Effect of rivet or bolt holes on the ultimate strength developed by 24S-T and alclad 75S-T sheet in incomplete diagonal tension /
by: Levin, L. Ross, et al.
Published: (1947)

A study on strength evaluations of EDNi/EDCu/NARloy-Z bonded joints /
by: Min, J. B.
Published: (1993)

Abrasion behavior of aluminum and composite skin coupons, stiffened skins, and stiffened panels representative of transport airplane structures /
by: Jackson, Karen E.
Published: (1985)

Research in structures, structural dynamics, and materials, 1989 : work-in-progress and other special presentation papers presented at the AIAA/ASME/ASCE/AHS/ASC 30th Structures, Structural Dynamics, and Materials Conference held in Mobile, Alabama, April 3-5, 1989 /
Published: (1989)

An experimental study of fatigue crack growth in aluminum sheet subjected to combined bending and membrane stresses /
by: Phillips, Edward P.
Published: (1997)

Three-dimensional cellular structures enhanced by shape memory alloys /
by: Nathal, Michael V.
Published: (2014)

Equivalent linearization analysis of geometrically nonlinear random vibrations using commercial finite element codes /
by: Rizzi, Stephen A. (Stephen Anthony)
Published: (2002)

Constitutive modeling for isotropic materials (HOST) /
Published: (1984)

Microstructure-property relationships in Al-Cu-Li-Ag-Mg Weldalite [superscript TM] alloys /
by: Langan, T. J., et al.
Published: (1991)

Moisture-induced alumina scale spallation : the hydrogen factor /
by: Smialek, James L.
Published: (2010)

Elastic response of (001)-oriented PWA 1480 single crystal : the influence of secondary orientation /
by: Kalluri, Sreeramesh
Published: (1991)