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You searched for +publisher:"Virginia Tech" +contributor:("Johnson, Eric R."). Showing records 1 – 30 of 101 total matches.

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1. Khan, Arafat Islam. Progressive Failure Analysis of Laminated Composite Structures.

Degree: PhD, Aerospace Engineering, 2015, Virginia Tech

 Laminated composite structures have started to play a very significant role in today's aircraft industry. The application of composite materials has now gone beyond the… (more)

Subjects/Keywords: Composites; Progressive Failure; Puck and Schürmann Failure Criteria; USDFLD; Laminated Structure

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APA (6th Edition):

Khan, A. I. (2015). Progressive Failure Analysis of Laminated Composite Structures. (Doctoral Dissertation). Virginia Tech. Retrieved from http://hdl.handle.net/10919/64389

Chicago Manual of Style (16th Edition):

Khan, Arafat Islam. “Progressive Failure Analysis of Laminated Composite Structures.” 2015. Doctoral Dissertation, Virginia Tech. Accessed April 16, 2021. http://hdl.handle.net/10919/64389.

MLA Handbook (7th Edition):

Khan, Arafat Islam. “Progressive Failure Analysis of Laminated Composite Structures.” 2015. Web. 16 Apr 2021.

Vancouver:

Khan AI. Progressive Failure Analysis of Laminated Composite Structures. [Internet] [Doctoral dissertation]. Virginia Tech; 2015. [cited 2021 Apr 16]. Available from: http://hdl.handle.net/10919/64389.

Council of Science Editors:

Khan AI. Progressive Failure Analysis of Laminated Composite Structures. [Doctoral Dissertation]. Virginia Tech; 2015. Available from: http://hdl.handle.net/10919/64389


Virginia Tech

2. Elseifi, Mohamed A. A new scheme for the optimum design of stiffened composite panels with geometric imperfections.

Degree: PhD, Aerospace and Ocean Engineering, 1998, Virginia Tech

 Thin walled stiffened composite panels, which are among the most utilized structural elements in engineering, possess the unfortunate property of being highly sensitive to geometrical… (more)

Subjects/Keywords: imperfections; manufacturing; composite materials; postbuckling; convex models; design optimization; genetic algorithms; nonlinear finite elements

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APA (6th Edition):

Elseifi, M. A. (1998). A new scheme for the optimum design of stiffened composite panels with geometric imperfections. (Doctoral Dissertation). Virginia Tech. Retrieved from http://hdl.handle.net/10919/29250

Chicago Manual of Style (16th Edition):

Elseifi, Mohamed A. “A new scheme for the optimum design of stiffened composite panels with geometric imperfections.” 1998. Doctoral Dissertation, Virginia Tech. Accessed April 16, 2021. http://hdl.handle.net/10919/29250.

MLA Handbook (7th Edition):

Elseifi, Mohamed A. “A new scheme for the optimum design of stiffened composite panels with geometric imperfections.” 1998. Web. 16 Apr 2021.

Vancouver:

Elseifi MA. A new scheme for the optimum design of stiffened composite panels with geometric imperfections. [Internet] [Doctoral dissertation]. Virginia Tech; 1998. [cited 2021 Apr 16]. Available from: http://hdl.handle.net/10919/29250.

Council of Science Editors:

Elseifi MA. A new scheme for the optimum design of stiffened composite panels with geometric imperfections. [Doctoral Dissertation]. Virginia Tech; 1998. Available from: http://hdl.handle.net/10919/29250


Virginia Tech

3. Kim, Yong Y. Flexural-Torsional Coupled Vibration of Rotating Beams Using Orthogonal Polynomials.

Degree: MS, Aerospace and Ocean Engineering, 2000, Virginia Tech

 Dynamic behavior of flexural-torsional coupled vibration of rotating beams using the Rayleigh-Ritz method with orthogonal polynomials as basis functions is studied. The present work starts… (more)

Subjects/Keywords: Rotating blade; Orthogonal polynomials; Rayleigh-Ritzm method; Natural frequency; Felxural-torsional coupled vibration

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APA (6th Edition):

Kim, Y. Y. (2000). Flexural-Torsional Coupled Vibration of Rotating Beams Using Orthogonal Polynomials. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/32616

Chicago Manual of Style (16th Edition):

Kim, Yong Y. “Flexural-Torsional Coupled Vibration of Rotating Beams Using Orthogonal Polynomials.” 2000. Masters Thesis, Virginia Tech. Accessed April 16, 2021. http://hdl.handle.net/10919/32616.

MLA Handbook (7th Edition):

Kim, Yong Y. “Flexural-Torsional Coupled Vibration of Rotating Beams Using Orthogonal Polynomials.” 2000. Web. 16 Apr 2021.

Vancouver:

Kim YY. Flexural-Torsional Coupled Vibration of Rotating Beams Using Orthogonal Polynomials. [Internet] [Masters thesis]. Virginia Tech; 2000. [cited 2021 Apr 16]. Available from: http://hdl.handle.net/10919/32616.

Council of Science Editors:

Kim YY. Flexural-Torsional Coupled Vibration of Rotating Beams Using Orthogonal Polynomials. [Masters Thesis]. Virginia Tech; 2000. Available from: http://hdl.handle.net/10919/32616


Virginia Tech

4. Foster, John L. Computation of interlaminar stresses from finite element solutions to plate theories.

Degree: MS, Aerospace Engineering, 1991, Virginia Tech

  Interlaminar stresses are estimated from plate theories by equilibrium. The elasticity equations of equilibrium are integrated with respect to the thickness coordinate z using… (more)

Subjects/Keywords: Laminated materials; LD5655.V855 1991.F687

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APA (6th Edition):

Foster, J. L. (1991). Computation of interlaminar stresses from finite element solutions to plate theories. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/35814

Chicago Manual of Style (16th Edition):

Foster, John L. “Computation of interlaminar stresses from finite element solutions to plate theories.” 1991. Masters Thesis, Virginia Tech. Accessed April 16, 2021. http://hdl.handle.net/10919/35814.

MLA Handbook (7th Edition):

Foster, John L. “Computation of interlaminar stresses from finite element solutions to plate theories.” 1991. Web. 16 Apr 2021.

Vancouver:

Foster JL. Computation of interlaminar stresses from finite element solutions to plate theories. [Internet] [Masters thesis]. Virginia Tech; 1991. [cited 2021 Apr 16]. Available from: http://hdl.handle.net/10919/35814.

Council of Science Editors:

Foster JL. Computation of interlaminar stresses from finite element solutions to plate theories. [Masters Thesis]. Virginia Tech; 1991. Available from: http://hdl.handle.net/10919/35814


Virginia Tech

5. Pèrez, José G. Energy Absorption and Progressive Failure Response of Composite Fuselage Frames.

Degree: MS, Aerospace and Ocean Engineering, 1999, Virginia Tech

 Vertical drop testing of transport aircraft fuselage sections indicates that the frames play a major role in the process of absorbing the impact energy in… (more)

Subjects/Keywords: Energy Absorption; Braided Composites; Fuselage Frames

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APA (6th Edition):

Pèrez, J. G. (1999). Energy Absorption and Progressive Failure Response of Composite Fuselage Frames. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/34447

Chicago Manual of Style (16th Edition):

Pèrez, José G. “Energy Absorption and Progressive Failure Response of Composite Fuselage Frames.” 1999. Masters Thesis, Virginia Tech. Accessed April 16, 2021. http://hdl.handle.net/10919/34447.

MLA Handbook (7th Edition):

Pèrez, José G. “Energy Absorption and Progressive Failure Response of Composite Fuselage Frames.” 1999. Web. 16 Apr 2021.

Vancouver:

Pèrez JG. Energy Absorption and Progressive Failure Response of Composite Fuselage Frames. [Internet] [Masters thesis]. Virginia Tech; 1999. [cited 2021 Apr 16]. Available from: http://hdl.handle.net/10919/34447.

Council of Science Editors:

Pèrez JG. Energy Absorption and Progressive Failure Response of Composite Fuselage Frames. [Masters Thesis]. Virginia Tech; 1999. Available from: http://hdl.handle.net/10919/34447


Virginia Tech

6. Pilkington, Lawrence O. Impact Response and Failure of a Textile Composite Fuselage Frame.

Degree: MS, Aerospace and Ocean Engineering, 2004, Virginia Tech

 Impact tests are performed on two circular circumferential frame segments using a drop tower apparatus. These frames have a nominal radius of 120 inches, a… (more)

Subjects/Keywords: textile composite; impact response; dynamic response; fuselage

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APA (6th Edition):

Pilkington, L. O. (2004). Impact Response and Failure of a Textile Composite Fuselage Frame. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/10059

Chicago Manual of Style (16th Edition):

Pilkington, Lawrence O. “Impact Response and Failure of a Textile Composite Fuselage Frame.” 2004. Masters Thesis, Virginia Tech. Accessed April 16, 2021. http://hdl.handle.net/10919/10059.

MLA Handbook (7th Edition):

Pilkington, Lawrence O. “Impact Response and Failure of a Textile Composite Fuselage Frame.” 2004. Web. 16 Apr 2021.

Vancouver:

Pilkington LO. Impact Response and Failure of a Textile Composite Fuselage Frame. [Internet] [Masters thesis]. Virginia Tech; 2004. [cited 2021 Apr 16]. Available from: http://hdl.handle.net/10919/10059.

Council of Science Editors:

Pilkington LO. Impact Response and Failure of a Textile Composite Fuselage Frame. [Masters Thesis]. Virginia Tech; 2004. Available from: http://hdl.handle.net/10919/10059


Virginia Tech

7. Chretien, Nicolas. Numerical Constitutive Models of Woven and Braided Textile Structural Composites.

Degree: MS, Aerospace and Ocean Engineering, 2002, Virginia Tech

 Equivalent, three-dimensional elastic moduli are determined from unit cell models of balanced plain weave, 2D braid, 2D triaxial braid and 4x4 twill textile composite materials… (more)

Subjects/Keywords: constitutive models; progressive failure; effective moduli; homogenization; woven and braided fabrics; textile structural composites; composite materials

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APA (6th Edition):

Chretien, N. (2002). Numerical Constitutive Models of Woven and Braided Textile Structural Composites. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/31902

Chicago Manual of Style (16th Edition):

Chretien, Nicolas. “Numerical Constitutive Models of Woven and Braided Textile Structural Composites.” 2002. Masters Thesis, Virginia Tech. Accessed April 16, 2021. http://hdl.handle.net/10919/31902.

MLA Handbook (7th Edition):

Chretien, Nicolas. “Numerical Constitutive Models of Woven and Braided Textile Structural Composites.” 2002. Web. 16 Apr 2021.

Vancouver:

Chretien N. Numerical Constitutive Models of Woven and Braided Textile Structural Composites. [Internet] [Masters thesis]. Virginia Tech; 2002. [cited 2021 Apr 16]. Available from: http://hdl.handle.net/10919/31902.

Council of Science Editors:

Chretien N. Numerical Constitutive Models of Woven and Braided Textile Structural Composites. [Masters Thesis]. Virginia Tech; 2002. Available from: http://hdl.handle.net/10919/31902


Virginia Tech

8. Barlas, Fatma Aylin. Variable complexity modeling of postbuckled stiffeners for delamination initiation.

Degree: MS, Aerospace Engineering, 1993, Virginia Tech

 Delamination at the free edge is analyzed as a mode of failure for uniaxial compression of postbuckled structural components. Analyses are performed for I-section stiffeners… (more)

Subjects/Keywords: Composite materials; LD5655.V855 1993.B374

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APA (6th Edition):

Barlas, F. A. (1993). Variable complexity modeling of postbuckled stiffeners for delamination initiation. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/45361

Chicago Manual of Style (16th Edition):

Barlas, Fatma Aylin. “Variable complexity modeling of postbuckled stiffeners for delamination initiation.” 1993. Masters Thesis, Virginia Tech. Accessed April 16, 2021. http://hdl.handle.net/10919/45361.

MLA Handbook (7th Edition):

Barlas, Fatma Aylin. “Variable complexity modeling of postbuckled stiffeners for delamination initiation.” 1993. Web. 16 Apr 2021.

Vancouver:

Barlas FA. Variable complexity modeling of postbuckled stiffeners for delamination initiation. [Internet] [Masters thesis]. Virginia Tech; 1993. [cited 2021 Apr 16]. Available from: http://hdl.handle.net/10919/45361.

Council of Science Editors:

Barlas FA. Variable complexity modeling of postbuckled stiffeners for delamination initiation. [Masters Thesis]. Virginia Tech; 1993. Available from: http://hdl.handle.net/10919/45361


Virginia Tech

9. Henderson, Bancroft W. An Exploratory Study of the Application of Carbon Nanotubes to Skin Friction Measurements.

Degree: MS, Aerospace and Ocean Engineering, 2004, Virginia Tech

 A small shear sensor utilizing an array of carbon nanotubes to support a sensor head was developed for use in steady, high speed, 2D flow.… (more)

Subjects/Keywords: fiber optic; skin friction; nanotubes; shear stress

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APA (6th Edition):

Henderson, B. W. (2004). An Exploratory Study of the Application of Carbon Nanotubes to Skin Friction Measurements. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/34119

Chicago Manual of Style (16th Edition):

Henderson, Bancroft W. “An Exploratory Study of the Application of Carbon Nanotubes to Skin Friction Measurements.” 2004. Masters Thesis, Virginia Tech. Accessed April 16, 2021. http://hdl.handle.net/10919/34119.

MLA Handbook (7th Edition):

Henderson, Bancroft W. “An Exploratory Study of the Application of Carbon Nanotubes to Skin Friction Measurements.” 2004. Web. 16 Apr 2021.

Vancouver:

Henderson BW. An Exploratory Study of the Application of Carbon Nanotubes to Skin Friction Measurements. [Internet] [Masters thesis]. Virginia Tech; 2004. [cited 2021 Apr 16]. Available from: http://hdl.handle.net/10919/34119.

Council of Science Editors:

Henderson BW. An Exploratory Study of the Application of Carbon Nanotubes to Skin Friction Measurements. [Masters Thesis]. Virginia Tech; 2004. Available from: http://hdl.handle.net/10919/34119


Virginia Tech

10. Simon, Joshua Cameron. Response and Failure of Adhesively Bonded Automotive Composite Structures under Impact Loads.

Degree: MS, Mechanical Engineering, 2004, Virginia Tech

 An experimental technique for conducting low speed impact of adhesively bonded automotive composite joints is presented. Based on the use of a modified drop tower,… (more)

Subjects/Keywords: Impact; Mode I; Mode II; Mixed-Mode I/II; Adhesive Joint; Composite; Unstable Growth; Stick-Slip; Fracture

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APA (6th Edition):

Simon, J. C. (2004). Response and Failure of Adhesively Bonded Automotive Composite Structures under Impact Loads. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/34881

Chicago Manual of Style (16th Edition):

Simon, Joshua Cameron. “Response and Failure of Adhesively Bonded Automotive Composite Structures under Impact Loads.” 2004. Masters Thesis, Virginia Tech. Accessed April 16, 2021. http://hdl.handle.net/10919/34881.

MLA Handbook (7th Edition):

Simon, Joshua Cameron. “Response and Failure of Adhesively Bonded Automotive Composite Structures under Impact Loads.” 2004. Web. 16 Apr 2021.

Vancouver:

Simon JC. Response and Failure of Adhesively Bonded Automotive Composite Structures under Impact Loads. [Internet] [Masters thesis]. Virginia Tech; 2004. [cited 2021 Apr 16]. Available from: http://hdl.handle.net/10919/34881.

Council of Science Editors:

Simon JC. Response and Failure of Adhesively Bonded Automotive Composite Structures under Impact Loads. [Masters Thesis]. Virginia Tech; 2004. Available from: http://hdl.handle.net/10919/34881


Virginia Tech

11. Uzman, Burak Jr. Thermal Analysis and Response of Grid-Stiffened Composite Panels.

Degree: MS, Engineering Science and Mechanics, 1997, Virginia Tech

 A study aimed at determining the thermal deformation response and thermal buckling loads of rectangular grid-stiffened composite panels is presented. Two edge conditions are considered… (more)

Subjects/Keywords: Grid; Stiffened; Buckling; Composite Panels

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APA (6th Edition):

Uzman, B. J. (1997). Thermal Analysis and Response of Grid-Stiffened Composite Panels. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/31381

Chicago Manual of Style (16th Edition):

Uzman, Burak Jr. “Thermal Analysis and Response of Grid-Stiffened Composite Panels.” 1997. Masters Thesis, Virginia Tech. Accessed April 16, 2021. http://hdl.handle.net/10919/31381.

MLA Handbook (7th Edition):

Uzman, Burak Jr. “Thermal Analysis and Response of Grid-Stiffened Composite Panels.” 1997. Web. 16 Apr 2021.

Vancouver:

Uzman BJ. Thermal Analysis and Response of Grid-Stiffened Composite Panels. [Internet] [Masters thesis]. Virginia Tech; 1997. [cited 2021 Apr 16]. Available from: http://hdl.handle.net/10919/31381.

Council of Science Editors:

Uzman BJ. Thermal Analysis and Response of Grid-Stiffened Composite Panels. [Masters Thesis]. Virginia Tech; 1997. Available from: http://hdl.handle.net/10919/31381


Virginia Tech

12. Dippold, Samuel Mark. Validation of the ULSAP Closed-Form Method for Ultimate Strength Analysis of Cross-Stiffened Panels.

Degree: MS, Aerospace and Ocean Engineering, 2005, Virginia Tech

 This thesis presents the results of 67 ABAQUS elasto-plastic Riks ultimate strength analyses of cross-stiffened panels. These panels cover a wide range of typical geometries.… (more)

Subjects/Keywords: Stiffened Panel Ultimate Strength; Finite Element Simulation Panel Collapse; Panel Buckling and Collapse

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APA (6th Edition):

Dippold, S. M. (2005). Validation of the ULSAP Closed-Form Method for Ultimate Strength Analysis of Cross-Stiffened Panels. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/33965

Chicago Manual of Style (16th Edition):

Dippold, Samuel Mark. “Validation of the ULSAP Closed-Form Method for Ultimate Strength Analysis of Cross-Stiffened Panels.” 2005. Masters Thesis, Virginia Tech. Accessed April 16, 2021. http://hdl.handle.net/10919/33965.

MLA Handbook (7th Edition):

Dippold, Samuel Mark. “Validation of the ULSAP Closed-Form Method for Ultimate Strength Analysis of Cross-Stiffened Panels.” 2005. Web. 16 Apr 2021.

Vancouver:

Dippold SM. Validation of the ULSAP Closed-Form Method for Ultimate Strength Analysis of Cross-Stiffened Panels. [Internet] [Masters thesis]. Virginia Tech; 2005. [cited 2021 Apr 16]. Available from: http://hdl.handle.net/10919/33965.

Council of Science Editors:

Dippold SM. Validation of the ULSAP Closed-Form Method for Ultimate Strength Analysis of Cross-Stiffened Panels. [Masters Thesis]. Virginia Tech; 2005. Available from: http://hdl.handle.net/10919/33965


Virginia Tech

13. Cooper, David E. (David Edward). Stresses and deformations in cross-ply composite tubes subjected to circumferential temperature gradients.

Degree: MS, Engineering Mechanics, 1985, Virginia Tech

  The stresses and deformations in cross-ply composite tubes subjected in circumferential temperature gradients are studied. The motivation behind the study is the anticipated use… (more)

Subjects/Keywords: Deformations (Mechanics); LD5655.V855 1985.C668

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APA (6th Edition):

Cooper, D. E. (. E. (1985). Stresses and deformations in cross-ply composite tubes subjected to circumferential temperature gradients. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/45556

Chicago Manual of Style (16th Edition):

Cooper, David E (David Edward). “Stresses and deformations in cross-ply composite tubes subjected to circumferential temperature gradients.” 1985. Masters Thesis, Virginia Tech. Accessed April 16, 2021. http://hdl.handle.net/10919/45556.

MLA Handbook (7th Edition):

Cooper, David E (David Edward). “Stresses and deformations in cross-ply composite tubes subjected to circumferential temperature gradients.” 1985. Web. 16 Apr 2021.

Vancouver:

Cooper DE(E. Stresses and deformations in cross-ply composite tubes subjected to circumferential temperature gradients. [Internet] [Masters thesis]. Virginia Tech; 1985. [cited 2021 Apr 16]. Available from: http://hdl.handle.net/10919/45556.

Council of Science Editors:

Cooper DE(E. Stresses and deformations in cross-ply composite tubes subjected to circumferential temperature gradients. [Masters Thesis]. Virginia Tech; 1985. Available from: http://hdl.handle.net/10919/45556


Virginia Tech

14. Raciti, Stefano. A twenty DOF element for nonlinear analysis of unsymmetrically laminated beams.

Degree: MS, Systems Engineering, 1987, Virginia Tech

 The purpose of this study was to develop a simple one- dimensional finite element for the nonlinear analysis of symmetrically and unsymmetrically laminated composite beams… (more)

Subjects/Keywords: Aircraft industry; LD5655.V855 1987.R327

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APA (6th Edition):

Raciti, S. (1987). A twenty DOF element for nonlinear analysis of unsymmetrically laminated beams. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/44062

Chicago Manual of Style (16th Edition):

Raciti, Stefano. “A twenty DOF element for nonlinear analysis of unsymmetrically laminated beams.” 1987. Masters Thesis, Virginia Tech. Accessed April 16, 2021. http://hdl.handle.net/10919/44062.

MLA Handbook (7th Edition):

Raciti, Stefano. “A twenty DOF element for nonlinear analysis of unsymmetrically laminated beams.” 1987. Web. 16 Apr 2021.

Vancouver:

Raciti S. A twenty DOF element for nonlinear analysis of unsymmetrically laminated beams. [Internet] [Masters thesis]. Virginia Tech; 1987. [cited 2021 Apr 16]. Available from: http://hdl.handle.net/10919/44062.

Council of Science Editors:

Raciti S. A twenty DOF element for nonlinear analysis of unsymmetrically laminated beams. [Masters Thesis]. Virginia Tech; 1987. Available from: http://hdl.handle.net/10919/44062


Virginia Tech

15. Whitfield, Cindy Carol. Steady and Unsteady Force and Moment Data on a DARPA2 Submarine.

Degree: MS, Aerospace and Ocean Engineering, 1999, Virginia Tech

 Steady and unsteady force and moment experiments were conducted in the Virginia Tech Stability wind tunnel using the Dynamic Plunge-Pitch-Roll (DyPPiR) model mount to perform… (more)

Subjects/Keywords: unsteady; force; moments; steady

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APA (6th Edition):

Whitfield, C. C. (1999). Steady and Unsteady Force and Moment Data on a DARPA2 Submarine. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/34333

Chicago Manual of Style (16th Edition):

Whitfield, Cindy Carol. “Steady and Unsteady Force and Moment Data on a DARPA2 Submarine.” 1999. Masters Thesis, Virginia Tech. Accessed April 16, 2021. http://hdl.handle.net/10919/34333.

MLA Handbook (7th Edition):

Whitfield, Cindy Carol. “Steady and Unsteady Force and Moment Data on a DARPA2 Submarine.” 1999. Web. 16 Apr 2021.

Vancouver:

Whitfield CC. Steady and Unsteady Force and Moment Data on a DARPA2 Submarine. [Internet] [Masters thesis]. Virginia Tech; 1999. [cited 2021 Apr 16]. Available from: http://hdl.handle.net/10919/34333.

Council of Science Editors:

Whitfield CC. Steady and Unsteady Force and Moment Data on a DARPA2 Submarine. [Masters Thesis]. Virginia Tech; 1999. Available from: http://hdl.handle.net/10919/34333


Virginia Tech

16. Ghose, Dhrubajyoti. Finite element formulation of a thin-walled beam with improved response to warping restraint.

Degree: MS, Aerospace and Ocean Engineering, 1991, Virginia Tech

  Linear elastic theory of torsion and flexure of thin-walled beams as developed by Vlasov and Timoshenko respectively are well known and commonly used in… (more)

Subjects/Keywords: Girders; LD5655.V855 1991.G567

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APA (6th Edition):

Ghose, D. (1991). Finite element formulation of a thin-walled beam with improved response to warping restraint. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/46129

Chicago Manual of Style (16th Edition):

Ghose, Dhrubajyoti. “Finite element formulation of a thin-walled beam with improved response to warping restraint.” 1991. Masters Thesis, Virginia Tech. Accessed April 16, 2021. http://hdl.handle.net/10919/46129.

MLA Handbook (7th Edition):

Ghose, Dhrubajyoti. “Finite element formulation of a thin-walled beam with improved response to warping restraint.” 1991. Web. 16 Apr 2021.

Vancouver:

Ghose D. Finite element formulation of a thin-walled beam with improved response to warping restraint. [Internet] [Masters thesis]. Virginia Tech; 1991. [cited 2021 Apr 16]. Available from: http://hdl.handle.net/10919/46129.

Council of Science Editors:

Ghose D. Finite element formulation of a thin-walled beam with improved response to warping restraint. [Masters Thesis]. Virginia Tech; 1991. Available from: http://hdl.handle.net/10919/46129


Virginia Tech

17. Lovejoy, Andrew Elwyn. Natural frequencies and an atlas of mode shapes for generally-laminated, thick, skew, trapezoidal plates.

Degree: MS, Aerospace Engineering, 1994, Virginia Tech

  Composite materials are increasingly finding use in structures, such as aircraft components, and thus, an accurate method of predicting response is required. Even laminated… (more)

Subjects/Keywords: Shear (Mechanics); LD5655.V855 1994.L6845

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APA (6th Edition):

Lovejoy, A. E. (1994). Natural frequencies and an atlas of mode shapes for generally-laminated, thick, skew, trapezoidal plates. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/42992

Chicago Manual of Style (16th Edition):

Lovejoy, Andrew Elwyn. “Natural frequencies and an atlas of mode shapes for generally-laminated, thick, skew, trapezoidal plates.” 1994. Masters Thesis, Virginia Tech. Accessed April 16, 2021. http://hdl.handle.net/10919/42992.

MLA Handbook (7th Edition):

Lovejoy, Andrew Elwyn. “Natural frequencies and an atlas of mode shapes for generally-laminated, thick, skew, trapezoidal plates.” 1994. Web. 16 Apr 2021.

Vancouver:

Lovejoy AE. Natural frequencies and an atlas of mode shapes for generally-laminated, thick, skew, trapezoidal plates. [Internet] [Masters thesis]. Virginia Tech; 1994. [cited 2021 Apr 16]. Available from: http://hdl.handle.net/10919/42992.

Council of Science Editors:

Lovejoy AE. Natural frequencies and an atlas of mode shapes for generally-laminated, thick, skew, trapezoidal plates. [Masters Thesis]. Virginia Tech; 1994. Available from: http://hdl.handle.net/10919/42992


Virginia Tech

18. Henderson, Joseph Lynn. Combined structural and manufacturing optimization of stiffened composite panels.

Degree: MS, Aerospace Engineering, 1996, Virginia Tech

  Manufacturing considerations have been incorporated into the design optimization of a blade-stiffened composite panel. For the manufacturing analysis, a one-dimensional resin film infusion model… (more)

Subjects/Keywords: composites; structures; manufacturing; design optimization; genetic algorithms; stiffened panels; LD5655.V855 1996.H463

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APA (6th Edition):

Henderson, J. L. (1996). Combined structural and manufacturing optimization of stiffened composite panels. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/44819

Chicago Manual of Style (16th Edition):

Henderson, Joseph Lynn. “Combined structural and manufacturing optimization of stiffened composite panels.” 1996. Masters Thesis, Virginia Tech. Accessed April 16, 2021. http://hdl.handle.net/10919/44819.

MLA Handbook (7th Edition):

Henderson, Joseph Lynn. “Combined structural and manufacturing optimization of stiffened composite panels.” 1996. Web. 16 Apr 2021.

Vancouver:

Henderson JL. Combined structural and manufacturing optimization of stiffened composite panels. [Internet] [Masters thesis]. Virginia Tech; 1996. [cited 2021 Apr 16]. Available from: http://hdl.handle.net/10919/44819.

Council of Science Editors:

Henderson JL. Combined structural and manufacturing optimization of stiffened composite panels. [Masters Thesis]. Virginia Tech; 1996. Available from: http://hdl.handle.net/10919/44819


Virginia Tech

19. Derian, Edward J. Large deformation dynamic bending of composite beams.

Degree: MS, Engineering Mechanics, 1985, Virginia Tech

  The large deformation response of composite beams subjected to a dynamic axial load was studied. The beams were loaded with a moderate amount of… (more)

Subjects/Keywords: Buckling (Mechanics); LD5655.V855 1985.D474

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APA (6th Edition):

Derian, E. J. (1985). Large deformation dynamic bending of composite beams. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/45678

Chicago Manual of Style (16th Edition):

Derian, Edward J. “Large deformation dynamic bending of composite beams.” 1985. Masters Thesis, Virginia Tech. Accessed April 16, 2021. http://hdl.handle.net/10919/45678.

MLA Handbook (7th Edition):

Derian, Edward J. “Large deformation dynamic bending of composite beams.” 1985. Web. 16 Apr 2021.

Vancouver:

Derian EJ. Large deformation dynamic bending of composite beams. [Internet] [Masters thesis]. Virginia Tech; 1985. [cited 2021 Apr 16]. Available from: http://hdl.handle.net/10919/45678.

Council of Science Editors:

Derian EJ. Large deformation dynamic bending of composite beams. [Masters Thesis]. Virginia Tech; 1985. Available from: http://hdl.handle.net/10919/45678


Virginia Tech

20. Derstine, Mark S. Combined mechanical loading of composite tubes.

Degree: MS, Engineering Mechanics, 1988, Virginia Tech

see document Advisors/Committee Members: Pindera, Marek-Jerzy (committeechair), Hyer, Michael W. (committee member), Johnson, Eric R. (committee member).

Subjects/Keywords: Laminated materials.; LD5655.V855 1988.D477

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APA (6th Edition):

Derstine, M. S. (1988). Combined mechanical loading of composite tubes. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/43841

Chicago Manual of Style (16th Edition):

Derstine, Mark S. “Combined mechanical loading of composite tubes.” 1988. Masters Thesis, Virginia Tech. Accessed April 16, 2021. http://hdl.handle.net/10919/43841.

MLA Handbook (7th Edition):

Derstine, Mark S. “Combined mechanical loading of composite tubes.” 1988. Web. 16 Apr 2021.

Vancouver:

Derstine MS. Combined mechanical loading of composite tubes. [Internet] [Masters thesis]. Virginia Tech; 1988. [cited 2021 Apr 16]. Available from: http://hdl.handle.net/10919/43841.

Council of Science Editors:

Derstine MS. Combined mechanical loading of composite tubes. [Masters Thesis]. Virginia Tech; 1988. Available from: http://hdl.handle.net/10919/43841


Virginia Tech

21. Fierling, Yannick P. H. Analysis of fiber-reinforced composite plates utilizing curvilinear fiber trajectories.

Degree: MS, Engineering Mechanics, 1995, Virginia Tech

  Four plates with centrally located circular holes were manufactured using a fiber placement technique. With two plates the fibers were steered around the holes… (more)

Subjects/Keywords: fiber plates; LD5655.V855 1995.F547

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APA (6th Edition):

Fierling, Y. P. H. (1995). Analysis of fiber-reinforced composite plates utilizing curvilinear fiber trajectories. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/40850

Chicago Manual of Style (16th Edition):

Fierling, Yannick P H. “Analysis of fiber-reinforced composite plates utilizing curvilinear fiber trajectories.” 1995. Masters Thesis, Virginia Tech. Accessed April 16, 2021. http://hdl.handle.net/10919/40850.

MLA Handbook (7th Edition):

Fierling, Yannick P H. “Analysis of fiber-reinforced composite plates utilizing curvilinear fiber trajectories.” 1995. Web. 16 Apr 2021.

Vancouver:

Fierling YPH. Analysis of fiber-reinforced composite plates utilizing curvilinear fiber trajectories. [Internet] [Masters thesis]. Virginia Tech; 1995. [cited 2021 Apr 16]. Available from: http://hdl.handle.net/10919/40850.

Council of Science Editors:

Fierling YPH. Analysis of fiber-reinforced composite plates utilizing curvilinear fiber trajectories. [Masters Thesis]. Virginia Tech; 1995. Available from: http://hdl.handle.net/10919/40850


Virginia Tech

22. Kapoor, Hitesh. Nonlinear Dynamic Response of Flexible Membrane Structures to Blast Loads.

Degree: MS, Aerospace and Ocean Engineering, 2005, Virginia Tech

 The present work describes the finite element (FE) modeling and dynamic response of lightweight, deployable shelters (tent) to large external blast loads. Flexible shelters have… (more)

Subjects/Keywords: shelters. blast loads; shells; membranes; structural dynamics; nonlinear static and dynamic analysis; flexible structures; finite element modeling

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APA (6th Edition):

Kapoor, H. (2005). Nonlinear Dynamic Response of Flexible Membrane Structures to Blast Loads. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/41238

Chicago Manual of Style (16th Edition):

Kapoor, Hitesh. “Nonlinear Dynamic Response of Flexible Membrane Structures to Blast Loads.” 2005. Masters Thesis, Virginia Tech. Accessed April 16, 2021. http://hdl.handle.net/10919/41238.

MLA Handbook (7th Edition):

Kapoor, Hitesh. “Nonlinear Dynamic Response of Flexible Membrane Structures to Blast Loads.” 2005. Web. 16 Apr 2021.

Vancouver:

Kapoor H. Nonlinear Dynamic Response of Flexible Membrane Structures to Blast Loads. [Internet] [Masters thesis]. Virginia Tech; 2005. [cited 2021 Apr 16]. Available from: http://hdl.handle.net/10919/41238.

Council of Science Editors:

Kapoor H. Nonlinear Dynamic Response of Flexible Membrane Structures to Blast Loads. [Masters Thesis]. Virginia Tech; 2005. Available from: http://hdl.handle.net/10919/41238


Virginia Tech

23. Grall, Bruno. Structural analysis of geodesically stiffened composite panels with variable stiffener distribution.

Degree: MS, Engineering Mechanics, 1992, Virginia Tech

  A computationally efficient analysis approach is developed to predict buckling load of geodesically stiffened composite panels under in-plane loads. The analysis procedure accounts for… (more)

Subjects/Keywords: Buckling (Mechanics); LD5655.V855 1992.G724

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APA (6th Edition):

Grall, B. (1992). Structural analysis of geodesically stiffened composite panels with variable stiffener distribution. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/46401

Chicago Manual of Style (16th Edition):

Grall, Bruno. “Structural analysis of geodesically stiffened composite panels with variable stiffener distribution.” 1992. Masters Thesis, Virginia Tech. Accessed April 16, 2021. http://hdl.handle.net/10919/46401.

MLA Handbook (7th Edition):

Grall, Bruno. “Structural analysis of geodesically stiffened composite panels with variable stiffener distribution.” 1992. Web. 16 Apr 2021.

Vancouver:

Grall B. Structural analysis of geodesically stiffened composite panels with variable stiffener distribution. [Internet] [Masters thesis]. Virginia Tech; 1992. [cited 2021 Apr 16]. Available from: http://hdl.handle.net/10919/46401.

Council of Science Editors:

Grall B. Structural analysis of geodesically stiffened composite panels with variable stiffener distribution. [Masters Thesis]. Virginia Tech; 1992. Available from: http://hdl.handle.net/10919/46401


Virginia Tech

24. Li, Jing. A Geometrically nonlinear curved beam theory and its finite element formulation.

Degree: MS, Aerospace and Ocean Engineering, 2000, Virginia Tech

 This thesis presents a geometrically exact curved beam theory, with the assumption that the cross-section remains rigid, and its finite element formulation/implementation. The theory provides… (more)

Subjects/Keywords: finite element; Curved beam; finite rotations; geometrically exact; geometrically nonlinear

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APA (6th Edition):

Li, J. (2000). A Geometrically nonlinear curved beam theory and its finite element formulation. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/31071

Chicago Manual of Style (16th Edition):

Li, Jing. “A Geometrically nonlinear curved beam theory and its finite element formulation.” 2000. Masters Thesis, Virginia Tech. Accessed April 16, 2021. http://hdl.handle.net/10919/31071.

MLA Handbook (7th Edition):

Li, Jing. “A Geometrically nonlinear curved beam theory and its finite element formulation.” 2000. Web. 16 Apr 2021.

Vancouver:

Li J. A Geometrically nonlinear curved beam theory and its finite element formulation. [Internet] [Masters thesis]. Virginia Tech; 2000. [cited 2021 Apr 16]. Available from: http://hdl.handle.net/10919/31071.

Council of Science Editors:

Li J. A Geometrically nonlinear curved beam theory and its finite element formulation. [Masters Thesis]. Virginia Tech; 2000. Available from: http://hdl.handle.net/10919/31071


Virginia Tech

25. Yanna, Marc-Gabriel. An investigation of flow-induced vibrations of a steam-generator tube.

Degree: MS, Engineering Mechanics, 1993, Virginia Tech

 A typical failure in a heat exchanger is the breakdown of a tube due to impact-sliding wear. We investigate the dynamic behavior of a tube… (more)

Subjects/Keywords: Steam-boilers; LD5655.V855 1993.Y362

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APA (6th Edition):

Yanna, M. (1993). An investigation of flow-induced vibrations of a steam-generator tube. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/43786

Chicago Manual of Style (16th Edition):

Yanna, Marc-Gabriel. “An investigation of flow-induced vibrations of a steam-generator tube.” 1993. Masters Thesis, Virginia Tech. Accessed April 16, 2021. http://hdl.handle.net/10919/43786.

MLA Handbook (7th Edition):

Yanna, Marc-Gabriel. “An investigation of flow-induced vibrations of a steam-generator tube.” 1993. Web. 16 Apr 2021.

Vancouver:

Yanna M. An investigation of flow-induced vibrations of a steam-generator tube. [Internet] [Masters thesis]. Virginia Tech; 1993. [cited 2021 Apr 16]. Available from: http://hdl.handle.net/10919/43786.

Council of Science Editors:

Yanna M. An investigation of flow-induced vibrations of a steam-generator tube. [Masters Thesis]. Virginia Tech; 1993. Available from: http://hdl.handle.net/10919/43786


Virginia Tech

26. Sensmeier, Mark D. (Mark David). Static and dynamic large deflection flexural response of graphite- epoxy beams.

Degree: MS, Engineering Science and Mechanics, 1987, Virginia Tech

  In support of crashworthiness studies of composite airframes, the present study was undertaken to understand the large deflection flexural response and failure of graphite-epoxy… (more)

Subjects/Keywords: Airplanes; LD5655.V855 1987.S467

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APA (6th Edition):

Sensmeier, M. D. (. D. (1987). Static and dynamic large deflection flexural response of graphite- epoxy beams. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/45895

Chicago Manual of Style (16th Edition):

Sensmeier, Mark D (Mark David). “Static and dynamic large deflection flexural response of graphite- epoxy beams.” 1987. Masters Thesis, Virginia Tech. Accessed April 16, 2021. http://hdl.handle.net/10919/45895.

MLA Handbook (7th Edition):

Sensmeier, Mark D (Mark David). “Static and dynamic large deflection flexural response of graphite- epoxy beams.” 1987. Web. 16 Apr 2021.

Vancouver:

Sensmeier MD(D. Static and dynamic large deflection flexural response of graphite- epoxy beams. [Internet] [Masters thesis]. Virginia Tech; 1987. [cited 2021 Apr 16]. Available from: http://hdl.handle.net/10919/45895.

Council of Science Editors:

Sensmeier MD(D. Static and dynamic large deflection flexural response of graphite- epoxy beams. [Masters Thesis]. Virginia Tech; 1987. Available from: http://hdl.handle.net/10919/45895


Virginia Tech

27. Vidussoni, Marco A. Global-local finite element analysis of laminated composites.

Degree: MS, Engineering Mechanics, 1988, Virginia Tech

  A Global-Local finite element approach was used to investigate the interlaminar stresses in laminated composite plates with a central circular hole. Detailed solutions were… (more)

Subjects/Keywords: Finite element method; LD5655.V855 1988.V528

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APA (6th Edition):

Vidussoni, M. A. (1988). Global-local finite element analysis of laminated composites. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/45966

Chicago Manual of Style (16th Edition):

Vidussoni, Marco A. “Global-local finite element analysis of laminated composites.” 1988. Masters Thesis, Virginia Tech. Accessed April 16, 2021. http://hdl.handle.net/10919/45966.

MLA Handbook (7th Edition):

Vidussoni, Marco A. “Global-local finite element analysis of laminated composites.” 1988. Web. 16 Apr 2021.

Vancouver:

Vidussoni MA. Global-local finite element analysis of laminated composites. [Internet] [Masters thesis]. Virginia Tech; 1988. [cited 2021 Apr 16]. Available from: http://hdl.handle.net/10919/45966.

Council of Science Editors:

Vidussoni MA. Global-local finite element analysis of laminated composites. [Masters Thesis]. Virginia Tech; 1988. Available from: http://hdl.handle.net/10919/45966


Virginia Tech

28. Hart, Daniel Constantine. Development of a Progressive Failure Finite Element Analysis For a Braided Composite Fuselage Frame.

Degree: MS, Aerospace and Ocean Engineering, 2002, Virginia Tech

 Short, J-section columns fabricated from a textile composite are tested in axial compression to study the modes of failure with and without local buckling occuring.The… (more)

Subjects/Keywords: fuselage frame; progressive failure; delamination; J-section frame; triaxial braid; crashworthiness; postbuckling

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APA (6th Edition):

Hart, D. C. (2002). Development of a Progressive Failure Finite Element Analysis For a Braided Composite Fuselage Frame. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/34026

Chicago Manual of Style (16th Edition):

Hart, Daniel Constantine. “Development of a Progressive Failure Finite Element Analysis For a Braided Composite Fuselage Frame.” 2002. Masters Thesis, Virginia Tech. Accessed April 16, 2021. http://hdl.handle.net/10919/34026.

MLA Handbook (7th Edition):

Hart, Daniel Constantine. “Development of a Progressive Failure Finite Element Analysis For a Braided Composite Fuselage Frame.” 2002. Web. 16 Apr 2021.

Vancouver:

Hart DC. Development of a Progressive Failure Finite Element Analysis For a Braided Composite Fuselage Frame. [Internet] [Masters thesis]. Virginia Tech; 2002. [cited 2021 Apr 16]. Available from: http://hdl.handle.net/10919/34026.

Council of Science Editors:

Hart DC. Development of a Progressive Failure Finite Element Analysis For a Braided Composite Fuselage Frame. [Masters Thesis]. Virginia Tech; 2002. Available from: http://hdl.handle.net/10919/34026


Virginia Tech

29. Parietti, Lucie. Micromechanical finite element model for constitutive elastoplastic analysis of unidirectional fiber-reinforced composites.

Degree: MS, Engineering Mechanics, 1994, Virginia Tech

 A micro mechanical finite element model to compute the overall instantaneous stiffness of fiber-reinforced composites in elastic-plastic response is presented. The model is applicable to… (more)

Subjects/Keywords: elastic analysis; LD5655.V855 1994.P374

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APA (6th Edition):

Parietti, L. (1994). Micromechanical finite element model for constitutive elastoplastic analysis of unidirectional fiber-reinforced composites. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/33713

Chicago Manual of Style (16th Edition):

Parietti, Lucie. “Micromechanical finite element model for constitutive elastoplastic analysis of unidirectional fiber-reinforced composites.” 1994. Masters Thesis, Virginia Tech. Accessed April 16, 2021. http://hdl.handle.net/10919/33713.

MLA Handbook (7th Edition):

Parietti, Lucie. “Micromechanical finite element model for constitutive elastoplastic analysis of unidirectional fiber-reinforced composites.” 1994. Web. 16 Apr 2021.

Vancouver:

Parietti L. Micromechanical finite element model for constitutive elastoplastic analysis of unidirectional fiber-reinforced composites. [Internet] [Masters thesis]. Virginia Tech; 1994. [cited 2021 Apr 16]. Available from: http://hdl.handle.net/10919/33713.

Council of Science Editors:

Parietti L. Micromechanical finite element model for constitutive elastoplastic analysis of unidirectional fiber-reinforced composites. [Masters Thesis]. Virginia Tech; 1994. Available from: http://hdl.handle.net/10919/33713


Virginia Tech

30. Eldred, Lloyd B. Solution of non-linear partial differential equations with the Chebyshev Spectral method.

Degree: MS, Aerospace and Ocean Engineering, 1989, Virginia Tech

  The Spectral method is a powerful numerical technique for solving engineering differential equations. The method is a specialization of the method of weighted residuals.… (more)

Subjects/Keywords: Differential equations - Nonlinear; LD5655.V855 1989.E434

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APA (6th Edition):

Eldred, L. B. (1989). Solution of non-linear partial differential equations with the Chebyshev Spectral method. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/45953

Chicago Manual of Style (16th Edition):

Eldred, Lloyd B. “Solution of non-linear partial differential equations with the Chebyshev Spectral method.” 1989. Masters Thesis, Virginia Tech. Accessed April 16, 2021. http://hdl.handle.net/10919/45953.

MLA Handbook (7th Edition):

Eldred, Lloyd B. “Solution of non-linear partial differential equations with the Chebyshev Spectral method.” 1989. Web. 16 Apr 2021.

Vancouver:

Eldred LB. Solution of non-linear partial differential equations with the Chebyshev Spectral method. [Internet] [Masters thesis]. Virginia Tech; 1989. [cited 2021 Apr 16]. Available from: http://hdl.handle.net/10919/45953.

Council of Science Editors:

Eldred LB. Solution of non-linear partial differential equations with the Chebyshev Spectral method. [Masters Thesis]. Virginia Tech; 1989. Available from: http://hdl.handle.net/10919/45953

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