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1

Formulation of an improved smeared stiffener theory for buckling analysis of grid-stiffened composite panels

Navin Jaunky, Norman F. Knight Jr, Damodar R. Ambur

Journal:

Composites Part B: Engineering

Year:

1996

Language:

english

File:

PDF, 669 KB

english, 1996

2

[American Institute of Aeronautics and Astronautics 19th AIAA Applied Aerodynamics Conference - Anaheim,CA,U.S.A. (11 June 2001 - 14 June 2001)] 19th AIAA Applied Aerodynamics Conference - Design, fabrication and testing of composite energy-absorbing keel beams for general aviation type aircraft

Kellas, Sotiris, Knight, Jr., Norman

Year:

2001

Language:

english

File:

PDF, 1.65 MB

english, 2001

3

Buckling analysis of anisotropic variable-curvature panels and shells

Navin Jaunky, Norman F. Knight Jr., Damodar R. Ambur

Journal:

Composite Structures

Year:

1998

Language:

english

File:

PDF, 1.04 MB

english, 1998

4

Nonlinear dynamic analysis of curved beams

Ahmed K. Noor, Norman F. Knight Jr.

Journal:

Computer Methods in Applied Mechanics and Engineering

Year:

1980

Language:

english

File:

PDF, 1.78 MB

english, 1980

5

Factors influencing nonlinear static response prediction and test-analysis correlation for composite panels

Norman F. Knight Jr

Journal:

Composite Structures

Year:

1994

Language:

english

File:

PDF, 1.74 MB

english, 1994

6

Situated Identities and Social Psychological Experimentation

C. Norman Alexander, Jr. and Gordon W. Knight

Journal:

Year:

1971

Language:

english

File:

PDF, 1.41 MB

english, 1971

7

A refined first-order shear-deformation theory and its justification by plane strain bending problem of laminated plates

Yunqian Qi, Norman F. Knight Jr

Journal:

International Journal of Solids and Structures

Year:

1996

Language:

english

File:

PDF, 1.18 MB

english, 1996

8

[American Institute of Aeronautics and Astronautics 39th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference and Exhibit - Long Beach,CA,U.S.A. (20 April 1998 - 23 April 1998)] 39th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference and Exhibit - Buckling analysis of anisotropic curved panels and shells with variable curvature

Jaunky, Navin, Knight, Jr., Norman, Ambur, Damodar

Language:

english

File:

PDF, 742 KB

english

9

[American Institute of Aeronautics and Astronautics 38th Structures, Structural Dynamics, and Materials Conference - Kissimmee,FL,U.S.A. (07 April 1997 - 10 April 1997)] 38th Structures, Structural Dynamics, and Materials Conference - Developments in cylindrical shell stability analysis

Knight, Jr., Norman, Starnes, Jr., James, Knight, Jr., Norman, Starnes, Jr., James

Year:

1997

Language:

english

File:

PDF, 1.69 MB

english, 1997

10

An assessment of shell theories for buckling ofcircular cylindrical laminated composite panels loaded inaxial compression

Navin Jaunky, Norman F. Knight Jr

Journal:

International Journal of Solids and Structures

Year:

1999

Language:

english

File:

PDF, 1.04 MB

english, 1999

11

[American Institute of Aeronautics and Astronautics 37th Structure, Structural Dynamics and Materials Conference - Salt Lake City,UT,U.S.A. (15 April 1996 - 17 April 1996)] 37th Structure, Structural Dynamics and Materials Conference - Optimal design of grid-stiffened composite panels using global and local buckling analyses

Jaunky, Navin, Knight, Jr., Norman, Ambur, Damodar

Year:

1996

Language:

english

File:

PDF, 973 KB

english, 1996

12

Numerical simulations for high-energy impact of thin plates

Damodar R. Ambur, Navin Jaunky, Robin E. Lawson, Norman F. Knight Jr.

Journal:

International Journal of Impact Engineering

Year:

2001

Language:

english

File:

PDF, 1.02 MB

english, 2001

13

[American Institute of Aeronautics and Astronautics 38th Structures, Structural Dynamics, and Materials Conference - Kissimmee,FL,U.S.A. (07 April 1997 - 10 April 1997)] 38th Structures, Structural Dynamics, and Materials Conference - Optimal design of general stiffened composite circular cylinders for global buckling with strength constraints

Jaunky, Navin, Knight, Jr., Norman, Ambur, Damodar, Jaunky, Navin, Knight, Jr., Norman, Ambur, Damodar

Language:

english

File:

PDF, 914 KB

english

14

[American Institute of Aeronautics and Astronautics 41st Structures, Structural Dynamics, and Materials Conference and Exhibit - Atlanta,GA,U.S.A. (03 April 2000 - 06 April 2000)] 41st Structures, Structural Dynamics, and Materials Conference and Exhibit - Controlling a nonlinear solution procedure during a progressive failure analysis

Knight, Jr., Norman, Rankin, Charles, Brogan, Frank

Language:

english

File:

PDF, 2.42 MB

english

15

[American Institute of Aeronautics and Astronautics 38th Structures, Structural Dynamics, and Materials Conference - Kissimmee,FL,U.S.A. (07 April 1997 - 10 April 1997)] 38th Structures, Structural Dynamics, and Materials Conference - Soft lattice truss static polynomial response using energy methods

Kenner, Winfred, Knight, Jr., Norman, Kenner, Winfred, Knight, Jr., Norman

Year:

1997

Language:

english

File:

PDF, 1015 KB

english, 1997

16

Penetration simulation for uncontained engine debris impact on fuselage-like panels using LS-DYNA

Norman F.Knight Jr, Navin Jaunky, Robin E Lawson, Damodar R Ambur

Journal:

Finite Elements in Analysis and Design

Year:

2000

Language:

english

File:

PDF, 2.91 MB

english, 2000

17

Improved assumed-stress hybrid shell element with drilling degrees of freedom for linear stress, buckling and free vibration analyses

Govind Rengarajan, Mohammad A. Aminpour, Norman F. Knight Jr.

Journal:

International Journal for Numerical Methods in Engineering

Year:

1995

Language:

english

File:

PDF, 1.18 MB

english, 1995

18

Global/local methods research using a common structural analysis framework

Norman F. Knight Jr., Jonathan B. Ransom, O.Hayden Griffin Jr., Danniella M. Thompson

Journal:

Finite Elements in Analysis and Design

Year:

1991

Language:

english

File:

PDF, 1.33 MB

english, 1991

19

Comparison of symbolic and numerical integration methods for an assumed-stress hybrid shell element

Govind Rengarajan, Norman F. Knight Jr., Mohammad A. Aminpour

Journal:

International Journal for Numerical Methods in Biomedical Engineering

Year:

1995

Language:

english

File:

PDF, 576 KB

english, 1995

20

[American Institute of Aeronautics and Astronautics 19th AIAA Applied Aerodynamics Conference - Anaheim,CA,U.S.A. (11 June 2001 - 14 June 2001)] 19th AIAA Applied Aerodynamics Conference - Controlling progressive failure analyses using artificial viscous damping

Knight, Jr., Norman, Rankin, Charles, Brogan, Frank

Year:

2001

File:

PDF, 1.21 MB

2001

21

[American Institute of Aeronautics and Astronautics 41st Structures, Structural Dynamics, and Materials Conference and Exhibit - Atlanta,GA,U.S.A. (03 April 2000 - 06 April 2000)] 41st Structures, Structural Dynamics, and Materials Conference and Exhibit - Predicting the impact response of an energy-absorbing composite subfloor beam

Knight, Jr., Norman, Kellas, Sotiris, Pinson, Larry

File:

PDF, 1.02 MB

22

[American Institute of Aeronautics and Astronautics 38th Structures, Structural Dynamics, and Materials Conference - Kissimmee,FL,U.S.A. (07 April 1997 - 10 April 1997)] 38th Structures, Structural Dynamics, and Materials Conference - Evaluation of a progressive failure analysis methodology for laminated composite structures

Sleight, David, Knight, Jr., Norman, Wang, John, Sleight, David, Knight, Jr., Norman, Wang, John

Year:

1997

Language:

english

File:

PDF, 1.55 MB

english, 1997

23

Adaptive dynamic relaxation algorithm for non-linear hyperelastic structures Part I. Formulation

David R. Oakley, Norman F. Knight Jr.

Journal:

Computer Methods in Applied Mechanics and Engineering

Year:

1995

Language:

english

File:

PDF, 1.24 MB

english, 1995

24

Restatement of first-order shear-deformation theory for laminated plates

Norman F. Knight Jr, Yunqian Qi

Journal:

International Journal of Solids and Structures

Year:

1997

Language:

english

File:

PDF, 883 KB

english, 1997

25

Adaptive dynamic relaxation algorithm for non-linear hyperelastic structures Part II. Single-processor implementation

David R. Oakley, Norman F. Knight Jr.

Journal:

Computer Methods in Applied Mechanics and Engineering

Year:

1995

Language:

english

File:

PDF, 895 KB

english, 1995

26

[American Institute of Aeronautics and Astronautics 40th Structures, Structural Dynamics, and Materials Conference and Exhibit - St. Louis,MO,U.S.A. (12 April 1999 - 15 April 1999)] 40th Structures, Structural Dynamics, and Materials Conference and Exhibit - Modeling and simulation for uncontained engine debris impact on fuselage skins using LS-DYNA3D

Knight, Jr., Norman, Jaunky, Navin, Lawson, Robin, Ambur, Damodar

Year:

1999

Language:

english

File:

PDF, 1.76 MB

english, 1999

27

Adaptive dynamic relaxation algorithm for non-linear hyperelastic structures Part III. Parallel implementation

David R. Oakley, Norman F. Knight Jr., Daniel D. Warner

Journal:

Computer Methods in Applied Mechanics and Engineering

Year:

1995

Language:

english

File:

PDF, 1.01 MB

english, 1995

28

STAGS computational procedure for progressive failure analysis of laminated composite structures

Norman F. Knight Jr., Charles C. Rankin, Frank A. Brogan

Journal:

International Journal of Non-Linear Mechanics

Year:

2002

Language:

english

File:

PDF, 868 KB

english, 2002

29

High-performance equation solvers and their impact on finite element analysis

Eugene L. Poole, Norman F. Knight Jr., D. Dale Davis Jr.

Journal:

International Journal for Numerical Methods in Engineering

Year:

1992

Language:

english

File:

PDF, 1.26 MB

english, 1992

30

[American Institute of Aeronautics and Astronautics 19th AIAA Applied Aerodynamics Conference - Anaheim,CA,U.S.A. (11 June 2001 - 14 June 2001)] 19th AIAA Applied Aerodynamics Conference - Low-velocity earth-penetration test and analysis

Fasanella, Edwin, Jones, Yvonne, Knight, Jr., Norman, Kellas, Sotiris

Language:

english

File:

PDF, 1.10 MB

english

31

[American Institute of Aeronautics and Astronautics 19th AIAA Applied Aerodynamics Conference - Anaheim,CA,U.S.A. (11 June 2001 - 14 June 2001)] 19th AIAA Applied Aerodynamics Conference - Controlling progressive failure analyses using artificial viscous damping

Knight, Jr., Norman, Rankin, Charles, Brogan, Frank

Year:

2001

Language:

english

File:

PDF, 1.21 MB

english, 2001

32

Assessment of structural analysis technology for static collapse of elastic cylindrical shells

Norman F. Knight Jr., Steven C. Macy, Susan L. McCleary

Journal:

Finite Elements in Analysis and Design

Year:

1995

Language:

english

File:

PDF, 1.86 MB

english, 1995

33

On a consistent first-order shear-deformation theory for laminated plates

Norman F. Knight Jr, Yunqian Qi

Journal:

Composites Part B: Engineering

Year:

1997

Language:

english

File:

PDF, 845 KB

english, 1997

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