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You searched for +publisher:"Old Dominion University" +contributor:("Osama A. Kandil"). Showing records 1 – 30 of 31 total matches.

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1. Erbas, Nurhak. Micron-Level Actuator for Thermal-Fluid Control in Microchannels.

Degree: PhD, Aerospace Engineering, 2006, Old Dominion University

  Effectiveness of an actuator is investigated for thermal-flow control in microchannels. First, simulations of a single actuator in a quiescent external medium are performed… (more)

Subjects/Keywords: Actuator; Microchannels; Micron-level; Thermal-fluid control; Mechanical Engineering; Navigation, Guidance, Control and Dynamics; Structures and Materials

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APA (6th Edition):

Erbas, N. (2006). Micron-Level Actuator for Thermal-Fluid Control in Microchannels. (Doctoral Dissertation). Old Dominion University. Retrieved from 9780542855351 ; https://digitalcommons.odu.edu/mae_etds/54

Chicago Manual of Style (16th Edition):

Erbas, Nurhak. “Micron-Level Actuator for Thermal-Fluid Control in Microchannels.” 2006. Doctoral Dissertation, Old Dominion University. Accessed December 05, 2020. 9780542855351 ; https://digitalcommons.odu.edu/mae_etds/54.

MLA Handbook (7th Edition):

Erbas, Nurhak. “Micron-Level Actuator for Thermal-Fluid Control in Microchannels.” 2006. Web. 05 Dec 2020.

Vancouver:

Erbas N. Micron-Level Actuator for Thermal-Fluid Control in Microchannels. [Internet] [Doctoral dissertation]. Old Dominion University; 2006. [cited 2020 Dec 05]. Available from: 9780542855351 ; https://digitalcommons.odu.edu/mae_etds/54.

Council of Science Editors:

Erbas N. Micron-Level Actuator for Thermal-Fluid Control in Microchannels. [Doctoral Dissertation]. Old Dominion University; 2006. Available from: 9780542855351 ; https://digitalcommons.odu.edu/mae_etds/54

2. Guo, Xinyun. Shape Memory Alloy Applications on Control of Thermal Buckling, Panel Flutter and Random Vibration of Composite Panels.

Degree: PhD, Mechanical & Aerospace Engineering, 2005, Old Dominion University

  Shape Memory Alloy (SMA) has a unique ability to recover large prestrain (up to 8∼10% elongation for Nitinol, a typical SMA material) completely when… (more)

Subjects/Keywords: Buckling; Composite panels; Panel flutter; Shape memory alloys; Vibration; Aerospace Engineering; Structures and Materials

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APA (6th Edition):

Guo, X. (2005). Shape Memory Alloy Applications on Control of Thermal Buckling, Panel Flutter and Random Vibration of Composite Panels. (Doctoral Dissertation). Old Dominion University. Retrieved from 9780542189166 ; https://digitalcommons.odu.edu/mae_etds/184

Chicago Manual of Style (16th Edition):

Guo, Xinyun. “Shape Memory Alloy Applications on Control of Thermal Buckling, Panel Flutter and Random Vibration of Composite Panels.” 2005. Doctoral Dissertation, Old Dominion University. Accessed December 05, 2020. 9780542189166 ; https://digitalcommons.odu.edu/mae_etds/184.

MLA Handbook (7th Edition):

Guo, Xinyun. “Shape Memory Alloy Applications on Control of Thermal Buckling, Panel Flutter and Random Vibration of Composite Panels.” 2005. Web. 05 Dec 2020.

Vancouver:

Guo X. Shape Memory Alloy Applications on Control of Thermal Buckling, Panel Flutter and Random Vibration of Composite Panels. [Internet] [Doctoral dissertation]. Old Dominion University; 2005. [cited 2020 Dec 05]. Available from: 9780542189166 ; https://digitalcommons.odu.edu/mae_etds/184.

Council of Science Editors:

Guo X. Shape Memory Alloy Applications on Control of Thermal Buckling, Panel Flutter and Random Vibration of Composite Panels. [Doctoral Dissertation]. Old Dominion University; 2005. Available from: 9780542189166 ; https://digitalcommons.odu.edu/mae_etds/184

3. Bayraktar, Ilhan. External Aerodynamics of Heavy Ground Vehicles: Computations and Wind Tunnel Testing.

Degree: PhD, Aerospace Engineering, 2002, Old Dominion University

  Aerodynamic characteristics of a ground vehicle affect vehicle operation in many ways. Aerodynamic drag, lift and side forces have influence on fuel efficiency, vehicle… (more)

Subjects/Keywords: Aerodynamics; Bluff body; Ground vehicles; Wind tunnel; Aerodynamics and Fluid Mechanics; Aerospace Engineering; Automotive Engineering; Mechanical Engineering

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APA (6th Edition):

Bayraktar, I. (2002). External Aerodynamics of Heavy Ground Vehicles: Computations and Wind Tunnel Testing. (Doctoral Dissertation). Old Dominion University. Retrieved from 9780493712970 ; https://digitalcommons.odu.edu/mae_etds/49

Chicago Manual of Style (16th Edition):

Bayraktar, Ilhan. “External Aerodynamics of Heavy Ground Vehicles: Computations and Wind Tunnel Testing.” 2002. Doctoral Dissertation, Old Dominion University. Accessed December 05, 2020. 9780493712970 ; https://digitalcommons.odu.edu/mae_etds/49.

MLA Handbook (7th Edition):

Bayraktar, Ilhan. “External Aerodynamics of Heavy Ground Vehicles: Computations and Wind Tunnel Testing.” 2002. Web. 05 Dec 2020.

Vancouver:

Bayraktar I. External Aerodynamics of Heavy Ground Vehicles: Computations and Wind Tunnel Testing. [Internet] [Doctoral dissertation]. Old Dominion University; 2002. [cited 2020 Dec 05]. Available from: 9780493712970 ; https://digitalcommons.odu.edu/mae_etds/49.

Council of Science Editors:

Bayraktar I. External Aerodynamics of Heavy Ground Vehicles: Computations and Wind Tunnel Testing. [Doctoral Dissertation]. Old Dominion University; 2002. Available from: 9780493712970 ; https://digitalcommons.odu.edu/mae_etds/49

4. Gecgel, Murat. Modeling and Simulation of Coaxial Helicopter Rotor Aerodynamics.

Degree: PhD, Aerospace Engineering, 2009, Old Dominion University

  A framework is developed for the computational fluid dynamics (CFD) analyses of a series of helicopter rotor flowfields in hover and in forward flight.… (more)

Subjects/Keywords: Coaxial rotors; Flowfields; Forward flight; Helicopter rotor; Aerodynamics and Fluid Mechanics; Aerospace Engineering

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APA (6th Edition):

Gecgel, M. (2009). Modeling and Simulation of Coaxial Helicopter Rotor Aerodynamics. (Doctoral Dissertation). Old Dominion University. Retrieved from 9781109566369 ; https://digitalcommons.odu.edu/mae_etds/53

Chicago Manual of Style (16th Edition):

Gecgel, Murat. “Modeling and Simulation of Coaxial Helicopter Rotor Aerodynamics.” 2009. Doctoral Dissertation, Old Dominion University. Accessed December 05, 2020. 9781109566369 ; https://digitalcommons.odu.edu/mae_etds/53.

MLA Handbook (7th Edition):

Gecgel, Murat. “Modeling and Simulation of Coaxial Helicopter Rotor Aerodynamics.” 2009. Web. 05 Dec 2020.

Vancouver:

Gecgel M. Modeling and Simulation of Coaxial Helicopter Rotor Aerodynamics. [Internet] [Doctoral dissertation]. Old Dominion University; 2009. [cited 2020 Dec 05]. Available from: 9781109566369 ; https://digitalcommons.odu.edu/mae_etds/53.

Council of Science Editors:

Gecgel M. Modeling and Simulation of Coaxial Helicopter Rotor Aerodynamics. [Doctoral Dissertation]. Old Dominion University; 2009. Available from: 9781109566369 ; https://digitalcommons.odu.edu/mae_etds/53

5. Kara, Kursat. Hypersonic Boundary Layer Receptivity to Acoustic Disturbances Over Cones.

Degree: PhD, Aerospace Engineering, 2008, Old Dominion University

  The receptivity mechanisms of hypersonic boundary layers to free stream acoustic disturbances are studied using both linear stability theory (LST) and direct numerical simulations… (more)

Subjects/Keywords: Acoustic disturbances; Cones; Hypersonic boundary layer; Aerospace Engineering; Engineering Mechanics; Plasma and Beam Physics

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APA (6th Edition):

Kara, K. (2008). Hypersonic Boundary Layer Receptivity to Acoustic Disturbances Over Cones. (Doctoral Dissertation). Old Dominion University. Retrieved from 9780549928584 ; https://digitalcommons.odu.edu/mae_etds/64

Chicago Manual of Style (16th Edition):

Kara, Kursat. “Hypersonic Boundary Layer Receptivity to Acoustic Disturbances Over Cones.” 2008. Doctoral Dissertation, Old Dominion University. Accessed December 05, 2020. 9780549928584 ; https://digitalcommons.odu.edu/mae_etds/64.

MLA Handbook (7th Edition):

Kara, Kursat. “Hypersonic Boundary Layer Receptivity to Acoustic Disturbances Over Cones.” 2008. Web. 05 Dec 2020.

Vancouver:

Kara K. Hypersonic Boundary Layer Receptivity to Acoustic Disturbances Over Cones. [Internet] [Doctoral dissertation]. Old Dominion University; 2008. [cited 2020 Dec 05]. Available from: 9780549928584 ; https://digitalcommons.odu.edu/mae_etds/64.

Council of Science Editors:

Kara K. Hypersonic Boundary Layer Receptivity to Acoustic Disturbances Over Cones. [Doctoral Dissertation]. Old Dominion University; 2008. Available from: 9780549928584 ; https://digitalcommons.odu.edu/mae_etds/64

6. Koklu, Mehti. Micro Synthetic Jets as Effective Actuator.

Degree: PhD, Aerospace Engineering, 2007, Old Dominion University

  Synthetic jets have previously been studied as actuators for external macroflow control and recently been proposed for internal microflow applications. Despite the wide variety… (more)

Subjects/Keywords: Effective actuator; Synthetic jets; Aerospace Engineering; Mechanical Engineering

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APA (6th Edition):

Koklu, M. (2007). Micro Synthetic Jets as Effective Actuator. (Doctoral Dissertation). Old Dominion University. Retrieved from 9780549069454 ; https://digitalcommons.odu.edu/mae_etds/70

Chicago Manual of Style (16th Edition):

Koklu, Mehti. “Micro Synthetic Jets as Effective Actuator.” 2007. Doctoral Dissertation, Old Dominion University. Accessed December 05, 2020. 9780549069454 ; https://digitalcommons.odu.edu/mae_etds/70.

MLA Handbook (7th Edition):

Koklu, Mehti. “Micro Synthetic Jets as Effective Actuator.” 2007. Web. 05 Dec 2020.

Vancouver:

Koklu M. Micro Synthetic Jets as Effective Actuator. [Internet] [Doctoral dissertation]. Old Dominion University; 2007. [cited 2020 Dec 05]. Available from: 9780549069454 ; https://digitalcommons.odu.edu/mae_etds/70.

Council of Science Editors:

Koklu M. Micro Synthetic Jets as Effective Actuator. [Doctoral Dissertation]. Old Dominion University; 2007. Available from: 9780549069454 ; https://digitalcommons.odu.edu/mae_etds/70

7. Khasdeo, Nitin. Sonic Boom Focusing Prediction and Delta Wing Shape Optimization for Boom Mitigation Studies.

Degree: PhD, Aerospace Engineering, 2007, Old Dominion University

  Supersonic travel over land would be a reality if new aircraft are designed such that they produce quieter ground sonic booms, no louder than… (more)

Subjects/Keywords: Boom mitigation; Focusing prediction; Sonic boom; Supersonic aircraft; Wing shape; Aerospace Engineering

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APA (6th Edition):

Khasdeo, N. (2007). Sonic Boom Focusing Prediction and Delta Wing Shape Optimization for Boom Mitigation Studies. (Doctoral Dissertation). Old Dominion University. Retrieved from 9780549329459 ; https://digitalcommons.odu.edu/mae_etds/72

Chicago Manual of Style (16th Edition):

Khasdeo, Nitin. “Sonic Boom Focusing Prediction and Delta Wing Shape Optimization for Boom Mitigation Studies.” 2007. Doctoral Dissertation, Old Dominion University. Accessed December 05, 2020. 9780549329459 ; https://digitalcommons.odu.edu/mae_etds/72.

MLA Handbook (7th Edition):

Khasdeo, Nitin. “Sonic Boom Focusing Prediction and Delta Wing Shape Optimization for Boom Mitigation Studies.” 2007. Web. 05 Dec 2020.

Vancouver:

Khasdeo N. Sonic Boom Focusing Prediction and Delta Wing Shape Optimization for Boom Mitigation Studies. [Internet] [Doctoral dissertation]. Old Dominion University; 2007. [cited 2020 Dec 05]. Available from: 9780549329459 ; https://digitalcommons.odu.edu/mae_etds/72.

Council of Science Editors:

Khasdeo N. Sonic Boom Focusing Prediction and Delta Wing Shape Optimization for Boom Mitigation Studies. [Doctoral Dissertation]. Old Dominion University; 2007. Available from: 9780549329459 ; https://digitalcommons.odu.edu/mae_etds/72

8. Mokhtar, Wael Ahmed. Boundary Interference Assessment and Correction for Open Jet Wind Tunnels Using Panel Methods.

Degree: PhD, Aerospace Engineering, 2006, Old Dominion University

  The presence of nearby boundaries in a wind tunnel can lead to aerodynamic measurements on a model in the wind tunnel that differ from… (more)

Subjects/Keywords: Boundary interference; Open jet; Wind tunnels; Aerospace Engineering; Mechanical Engineering; Structures and Materials

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APA (6th Edition):

Mokhtar, W. A. (2006). Boundary Interference Assessment and Correction for Open Jet Wind Tunnels Using Panel Methods. (Doctoral Dissertation). Old Dominion University. Retrieved from 9780542753879 ; https://digitalcommons.odu.edu/mae_etds/74

Chicago Manual of Style (16th Edition):

Mokhtar, Wael Ahmed. “Boundary Interference Assessment and Correction for Open Jet Wind Tunnels Using Panel Methods.” 2006. Doctoral Dissertation, Old Dominion University. Accessed December 05, 2020. 9780542753879 ; https://digitalcommons.odu.edu/mae_etds/74.

MLA Handbook (7th Edition):

Mokhtar, Wael Ahmed. “Boundary Interference Assessment and Correction for Open Jet Wind Tunnels Using Panel Methods.” 2006. Web. 05 Dec 2020.

Vancouver:

Mokhtar WA. Boundary Interference Assessment and Correction for Open Jet Wind Tunnels Using Panel Methods. [Internet] [Doctoral dissertation]. Old Dominion University; 2006. [cited 2020 Dec 05]. Available from: 9780542753879 ; https://digitalcommons.odu.edu/mae_etds/74.

Council of Science Editors:

Mokhtar WA. Boundary Interference Assessment and Correction for Open Jet Wind Tunnels Using Panel Methods. [Doctoral Dissertation]. Old Dominion University; 2006. Available from: 9780542753879 ; https://digitalcommons.odu.edu/mae_etds/74

9. Owis, Farouk. Jet Stability and Noise Computations Using Direct Numerical Simulation.

Degree: PhD, Aerospace Engineering, 1999, Old Dominion University

  The computations of axisymmetric jet noise with symmetric disturbances are investigated using the direct numerical simulation of the unsteady compressible Navier-Stokes equations. High order… (more)

Subjects/Keywords: Jet stability; Noise computations; Aerospace Engineering; Structures and Materials

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APA (6th Edition):

Owis, F. (1999). Jet Stability and Noise Computations Using Direct Numerical Simulation. (Doctoral Dissertation). Old Dominion University. Retrieved from 9780599525108 ; https://digitalcommons.odu.edu/mae_etds/80

Chicago Manual of Style (16th Edition):

Owis, Farouk. “Jet Stability and Noise Computations Using Direct Numerical Simulation.” 1999. Doctoral Dissertation, Old Dominion University. Accessed December 05, 2020. 9780599525108 ; https://digitalcommons.odu.edu/mae_etds/80.

MLA Handbook (7th Edition):

Owis, Farouk. “Jet Stability and Noise Computations Using Direct Numerical Simulation.” 1999. Web. 05 Dec 2020.

Vancouver:

Owis F. Jet Stability and Noise Computations Using Direct Numerical Simulation. [Internet] [Doctoral dissertation]. Old Dominion University; 1999. [cited 2020 Dec 05]. Available from: 9780599525108 ; https://digitalcommons.odu.edu/mae_etds/80.

Council of Science Editors:

Owis F. Jet Stability and Noise Computations Using Direct Numerical Simulation. [Doctoral Dissertation]. Old Dominion University; 1999. Available from: 9780599525108 ; https://digitalcommons.odu.edu/mae_etds/80

10. Yagiz, Bedri. Active Control of Shocks and Sonic Boom Ground Signal.

Degree: PhD, Aerospace Engineering, 2010, Old Dominion University

  The manipulation of a flow field to obtain a desired change is a much heightened subject. Active flow control has been the subject of… (more)

Subjects/Keywords: Active control; Shock waves; Sonic booms; Transonic flow; Aerospace Engineering

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APA (6th Edition):

Yagiz, B. (2010). Active Control of Shocks and Sonic Boom Ground Signal. (Doctoral Dissertation). Old Dominion University. Retrieved from 9781124504278 ; https://digitalcommons.odu.edu/mae_etds/92

Chicago Manual of Style (16th Edition):

Yagiz, Bedri. “Active Control of Shocks and Sonic Boom Ground Signal.” 2010. Doctoral Dissertation, Old Dominion University. Accessed December 05, 2020. 9781124504278 ; https://digitalcommons.odu.edu/mae_etds/92.

MLA Handbook (7th Edition):

Yagiz, Bedri. “Active Control of Shocks and Sonic Boom Ground Signal.” 2010. Web. 05 Dec 2020.

Vancouver:

Yagiz B. Active Control of Shocks and Sonic Boom Ground Signal. [Internet] [Doctoral dissertation]. Old Dominion University; 2010. [cited 2020 Dec 05]. Available from: 9781124504278 ; https://digitalcommons.odu.edu/mae_etds/92.

Council of Science Editors:

Yagiz B. Active Control of Shocks and Sonic Boom Ground Signal. [Doctoral Dissertation]. Old Dominion University; 2010. Available from: 9781124504278 ; https://digitalcommons.odu.edu/mae_etds/92

11. Yang, Zhi. Active and Adaptive Flow Control of Twin-Tail Buffet and Applications.

Degree: PhD, Aerospace Engineering, 2002, Old Dominion University

  Modern fighter aircraft with dual vertical tails are operated at high angles of attack. The vortex generated by leading edge extension (LEX) breaks down… (more)

Subjects/Keywords: Active flow control; Adaptive flow control; Twin-tail buffet; Aerodynamics and Fluid Mechanics; Aerospace Engineering; Structures and Materials

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APA (6th Edition):

Yang, Z. (2002). Active and Adaptive Flow Control of Twin-Tail Buffet and Applications. (Doctoral Dissertation). Old Dominion University. Retrieved from 9780493976112 ; https://digitalcommons.odu.edu/mae_etds/94

Chicago Manual of Style (16th Edition):

Yang, Zhi. “Active and Adaptive Flow Control of Twin-Tail Buffet and Applications.” 2002. Doctoral Dissertation, Old Dominion University. Accessed December 05, 2020. 9780493976112 ; https://digitalcommons.odu.edu/mae_etds/94.

MLA Handbook (7th Edition):

Yang, Zhi. “Active and Adaptive Flow Control of Twin-Tail Buffet and Applications.” 2002. Web. 05 Dec 2020.

Vancouver:

Yang Z. Active and Adaptive Flow Control of Twin-Tail Buffet and Applications. [Internet] [Doctoral dissertation]. Old Dominion University; 2002. [cited 2020 Dec 05]. Available from: 9780493976112 ; https://digitalcommons.odu.edu/mae_etds/94.

Council of Science Editors:

Yang Z. Active and Adaptive Flow Control of Twin-Tail Buffet and Applications. [Doctoral Dissertation]. Old Dominion University; 2002. Available from: 9780493976112 ; https://digitalcommons.odu.edu/mae_etds/94

12. Zhao, Hongwu. Hypersonic Boundary-Layer Stability Across a Compression Corner.

Degree: PhD, Aerospace Engineering, 2003, Old Dominion University

  Stability of a hypersonic boundary-layer over a compression corner was investigated numerically. The three-dimensional compressible Navier-Stokes equations were solved using a fifth-order weighted essentially… (more)

Subjects/Keywords: Boundary layer; Compression; Hypersoni; Turbulence; Aerospace Engineering

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APA (6th Edition):

Zhao, H. (2003). Hypersonic Boundary-Layer Stability Across a Compression Corner. (Doctoral Dissertation). Old Dominion University. Retrieved from https://digitalcommons.odu.edu/mae_etds/96

Chicago Manual of Style (16th Edition):

Zhao, Hongwu. “Hypersonic Boundary-Layer Stability Across a Compression Corner.” 2003. Doctoral Dissertation, Old Dominion University. Accessed December 05, 2020. https://digitalcommons.odu.edu/mae_etds/96.

MLA Handbook (7th Edition):

Zhao, Hongwu. “Hypersonic Boundary-Layer Stability Across a Compression Corner.” 2003. Web. 05 Dec 2020.

Vancouver:

Zhao H. Hypersonic Boundary-Layer Stability Across a Compression Corner. [Internet] [Doctoral dissertation]. Old Dominion University; 2003. [cited 2020 Dec 05]. Available from: https://digitalcommons.odu.edu/mae_etds/96.

Council of Science Editors:

Zhao H. Hypersonic Boundary-Layer Stability Across a Compression Corner. [Doctoral Dissertation]. Old Dominion University; 2003. Available from: https://digitalcommons.odu.edu/mae_etds/96

13. Sharaf El-Din, Hazem. Simulation of Active Control of Asymmetric Flows Around Slender Pointed Forebodies.

Degree: PhD, Mechanical & Aerospace Engineering, 1994, Old Dominion University

  At high angles of attack, the flowfield over slender forebodies becomes asymmetric with substantial side force, which may exceed the available control capability. The… (more)

Subjects/Keywords: Flow control; Asymmetric flows; Gases; Navier-Stokes equations; Aerospace Engineering; Fluid Dynamics; Mechanical Engineering

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APA (6th Edition):

Sharaf El-Din, H. (1994). Simulation of Active Control of Asymmetric Flows Around Slender Pointed Forebodies. (Doctoral Dissertation). Old Dominion University. Retrieved from https://digitalcommons.odu.edu/mae_etds/267

Chicago Manual of Style (16th Edition):

Sharaf El-Din, Hazem. “Simulation of Active Control of Asymmetric Flows Around Slender Pointed Forebodies.” 1994. Doctoral Dissertation, Old Dominion University. Accessed December 05, 2020. https://digitalcommons.odu.edu/mae_etds/267.

MLA Handbook (7th Edition):

Sharaf El-Din, Hazem. “Simulation of Active Control of Asymmetric Flows Around Slender Pointed Forebodies.” 1994. Web. 05 Dec 2020.

Vancouver:

Sharaf El-Din H. Simulation of Active Control of Asymmetric Flows Around Slender Pointed Forebodies. [Internet] [Doctoral dissertation]. Old Dominion University; 1994. [cited 2020 Dec 05]. Available from: https://digitalcommons.odu.edu/mae_etds/267.

Council of Science Editors:

Sharaf El-Din H. Simulation of Active Control of Asymmetric Flows Around Slender Pointed Forebodies. [Doctoral Dissertation]. Old Dominion University; 1994. Available from: https://digitalcommons.odu.edu/mae_etds/267

14. Salman, Ahmed Abd-El-Bar Ahmed. Unsteady Euler and Navier-Stokes Computations Around Oscillating Delta Wing Including Dynamics.

Degree: PhD, Mechanical & Aerospace Engineering, 1992, Old Dominion University

  Unsteady flows around rigid or flexible delta wings with and without oscillating leading-edge flaps are considered. These unsteady flow problems are categorized under two… (more)

Subjects/Keywords: Euler equations; Navier-Stokes equations; Viscous flow; Aerospace Engineering; Mechanical Engineering

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APA (6th Edition):

Salman, A. A. A. (1992). Unsteady Euler and Navier-Stokes Computations Around Oscillating Delta Wing Including Dynamics. (Doctoral Dissertation). Old Dominion University. Retrieved from https://digitalcommons.odu.edu/mae_etds/268

Chicago Manual of Style (16th Edition):

Salman, Ahmed Abd-El-Bar Ahmed. “Unsteady Euler and Navier-Stokes Computations Around Oscillating Delta Wing Including Dynamics.” 1992. Doctoral Dissertation, Old Dominion University. Accessed December 05, 2020. https://digitalcommons.odu.edu/mae_etds/268.

MLA Handbook (7th Edition):

Salman, Ahmed Abd-El-Bar Ahmed. “Unsteady Euler and Navier-Stokes Computations Around Oscillating Delta Wing Including Dynamics.” 1992. Web. 05 Dec 2020.

Vancouver:

Salman AAA. Unsteady Euler and Navier-Stokes Computations Around Oscillating Delta Wing Including Dynamics. [Internet] [Doctoral dissertation]. Old Dominion University; 1992. [cited 2020 Dec 05]. Available from: https://digitalcommons.odu.edu/mae_etds/268.

Council of Science Editors:

Salman AAA. Unsteady Euler and Navier-Stokes Computations Around Oscillating Delta Wing Including Dynamics. [Doctoral Dissertation]. Old Dominion University; 1992. Available from: https://digitalcommons.odu.edu/mae_etds/268

15. Wong, Tin-Chee. Prediction and Control of Asymmetric Vortical Flows Around Slender Bodies Using Navier-Stokes Equations.

Degree: PhD, Mechanical & Aerospace Engineering, 1991, Old Dominion University

  Steady and unsteady vortex-dominated flows around slender bodies at high angles of attack are solved using the unsteady, compressible Navier-Stokes equations. An implicit upwind,… (more)

Subjects/Keywords: Vortical flows; Navier-Stokes equations; Unsteady flow; Aerospace Engineering; Mechanical Engineering

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APA (6th Edition):

Wong, T. (1991). Prediction and Control of Asymmetric Vortical Flows Around Slender Bodies Using Navier-Stokes Equations. (Doctoral Dissertation). Old Dominion University. Retrieved from https://digitalcommons.odu.edu/mae_etds/291

Chicago Manual of Style (16th Edition):

Wong, Tin-Chee. “Prediction and Control of Asymmetric Vortical Flows Around Slender Bodies Using Navier-Stokes Equations.” 1991. Doctoral Dissertation, Old Dominion University. Accessed December 05, 2020. https://digitalcommons.odu.edu/mae_etds/291.

MLA Handbook (7th Edition):

Wong, Tin-Chee. “Prediction and Control of Asymmetric Vortical Flows Around Slender Bodies Using Navier-Stokes Equations.” 1991. Web. 05 Dec 2020.

Vancouver:

Wong T. Prediction and Control of Asymmetric Vortical Flows Around Slender Bodies Using Navier-Stokes Equations. [Internet] [Doctoral dissertation]. Old Dominion University; 1991. [cited 2020 Dec 05]. Available from: https://digitalcommons.odu.edu/mae_etds/291.

Council of Science Editors:

Wong T. Prediction and Control of Asymmetric Vortical Flows Around Slender Bodies Using Navier-Stokes Equations. [Doctoral Dissertation]. Old Dominion University; 1991. Available from: https://digitalcommons.odu.edu/mae_etds/291

16. Yen, Guan-Wei. Unsteady Flow Simulations About Moving Boundary Configurations Using Dynamic Domain Decomposition Techniques.

Degree: PhD, Mechanical & Aerospace Engineering, 1994, Old Dominion University

  A computational method is developed to solve the coupled governing equations of an unsteady flowfield and those of rigid-body dynamics in six degrees-of-freedom (6-DOF).… (more)

Subjects/Keywords: Unsteady flow; Navier-Stokes equations; Gases; Applied Mechanics; Fluid Dynamics; Structures and Materials

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APA (6th Edition):

Yen, G. (1994). Unsteady Flow Simulations About Moving Boundary Configurations Using Dynamic Domain Decomposition Techniques. (Doctoral Dissertation). Old Dominion University. Retrieved from https://digitalcommons.odu.edu/mae_etds/296

Chicago Manual of Style (16th Edition):

Yen, Guan-Wei. “Unsteady Flow Simulations About Moving Boundary Configurations Using Dynamic Domain Decomposition Techniques.” 1994. Doctoral Dissertation, Old Dominion University. Accessed December 05, 2020. https://digitalcommons.odu.edu/mae_etds/296.

MLA Handbook (7th Edition):

Yen, Guan-Wei. “Unsteady Flow Simulations About Moving Boundary Configurations Using Dynamic Domain Decomposition Techniques.” 1994. Web. 05 Dec 2020.

Vancouver:

Yen G. Unsteady Flow Simulations About Moving Boundary Configurations Using Dynamic Domain Decomposition Techniques. [Internet] [Doctoral dissertation]. Old Dominion University; 1994. [cited 2020 Dec 05]. Available from: https://digitalcommons.odu.edu/mae_etds/296.

Council of Science Editors:

Yen G. Unsteady Flow Simulations About Moving Boundary Configurations Using Dynamic Domain Decomposition Techniques. [Doctoral Dissertation]. Old Dominion University; 1994. Available from: https://digitalcommons.odu.edu/mae_etds/296

17. Zheng, Zhongquan Charlie. The Influence of Reynolds Number and Atmospheric Effects on Aircraft Wake Vortices Near the Ground.

Degree: PhD, Mechanical & Aerospace Engineering, 1993, Old Dominion University

  Aircraft wakes represent potential hazards which can control aircraft spacing and thus limit airport capacity. Wake vortex trajectories and strengths are altered radically by… (more)

Subjects/Keywords: Wakes; Reynolds number; Vortex-motion; Aerospace Engineering; Applied Mechanics

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APA (6th Edition):

Zheng, Z. C. (1993). The Influence of Reynolds Number and Atmospheric Effects on Aircraft Wake Vortices Near the Ground. (Doctoral Dissertation). Old Dominion University. Retrieved from https://digitalcommons.odu.edu/mae_etds/297

Chicago Manual of Style (16th Edition):

Zheng, Zhongquan Charlie. “The Influence of Reynolds Number and Atmospheric Effects on Aircraft Wake Vortices Near the Ground.” 1993. Doctoral Dissertation, Old Dominion University. Accessed December 05, 2020. https://digitalcommons.odu.edu/mae_etds/297.

MLA Handbook (7th Edition):

Zheng, Zhongquan Charlie. “The Influence of Reynolds Number and Atmospheric Effects on Aircraft Wake Vortices Near the Ground.” 1993. Web. 05 Dec 2020.

Vancouver:

Zheng ZC. The Influence of Reynolds Number and Atmospheric Effects on Aircraft Wake Vortices Near the Ground. [Internet] [Doctoral dissertation]. Old Dominion University; 1993. [cited 2020 Dec 05]. Available from: https://digitalcommons.odu.edu/mae_etds/297.

Council of Science Editors:

Zheng ZC. The Influence of Reynolds Number and Atmospheric Effects on Aircraft Wake Vortices Near the Ground. [Doctoral Dissertation]. Old Dominion University; 1993. Available from: https://digitalcommons.odu.edu/mae_etds/297

18. Rose, Ollie James. Curvilinear Interface Methodology for Finite-Element Applications.

Degree: PhD, Mechanical & Aerospace Engineering, 2000, Old Dominion University

  Recent trends in design and manufacturing suggest a tendency toward multiple centers of specialty which results in a need for improved integration methodology for… (more)

Subjects/Keywords: Automatic grid interfacing; Curvilinear interface; Finite element applications; Multiple independent subdomains; Aerospace Engineering; Mechanical Engineering

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APA (6th Edition):

Rose, O. J. (2000). Curvilinear Interface Methodology for Finite-Element Applications. (Doctoral Dissertation). Old Dominion University. Retrieved from 9780493177960 ; https://digitalcommons.odu.edu/mae_etds/192

Chicago Manual of Style (16th Edition):

Rose, Ollie James. “Curvilinear Interface Methodology for Finite-Element Applications.” 2000. Doctoral Dissertation, Old Dominion University. Accessed December 05, 2020. 9780493177960 ; https://digitalcommons.odu.edu/mae_etds/192.

MLA Handbook (7th Edition):

Rose, Ollie James. “Curvilinear Interface Methodology for Finite-Element Applications.” 2000. Web. 05 Dec 2020.

Vancouver:

Rose OJ. Curvilinear Interface Methodology for Finite-Element Applications. [Internet] [Doctoral dissertation]. Old Dominion University; 2000. [cited 2020 Dec 05]. Available from: 9780493177960 ; https://digitalcommons.odu.edu/mae_etds/192.

Council of Science Editors:

Rose OJ. Curvilinear Interface Methodology for Finite-Element Applications. [Doctoral Dissertation]. Old Dominion University; 2000. Available from: 9780493177960 ; https://digitalcommons.odu.edu/mae_etds/192

19. Chu, Li-Chuan. Integral Equation Solution of the Full Potential Equation for Three-Dimensional, Steady, Transonic Wing Flows.

Degree: PhD, Mechanical & Aerospace Engineering, 1988, Old Dominion University

  An integral equation method for solving the full potential equation has been developed for three dimensional transonic vortex-wing flows. This method is capable of… (more)

Subjects/Keywords: Integral equation method; Transonic wing flows; Murman-Cole type; Mechanical Engineering

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APA (6th Edition):

Chu, L. (1988). Integral Equation Solution of the Full Potential Equation for Three-Dimensional, Steady, Transonic Wing Flows. (Doctoral Dissertation). Old Dominion University. Retrieved from https://digitalcommons.odu.edu/mae_etds/222

Chicago Manual of Style (16th Edition):

Chu, Li-Chuan. “Integral Equation Solution of the Full Potential Equation for Three-Dimensional, Steady, Transonic Wing Flows.” 1988. Doctoral Dissertation, Old Dominion University. Accessed December 05, 2020. https://digitalcommons.odu.edu/mae_etds/222.

MLA Handbook (7th Edition):

Chu, Li-Chuan. “Integral Equation Solution of the Full Potential Equation for Three-Dimensional, Steady, Transonic Wing Flows.” 1988. Web. 05 Dec 2020.

Vancouver:

Chu L. Integral Equation Solution of the Full Potential Equation for Three-Dimensional, Steady, Transonic Wing Flows. [Internet] [Doctoral dissertation]. Old Dominion University; 1988. [cited 2020 Dec 05]. Available from: https://digitalcommons.odu.edu/mae_etds/222.

Council of Science Editors:

Chu L. Integral Equation Solution of the Full Potential Equation for Three-Dimensional, Steady, Transonic Wing Flows. [Doctoral Dissertation]. Old Dominion University; 1988. Available from: https://digitalcommons.odu.edu/mae_etds/222

20. Cannizzaro, Frank E. Runge-Kutta Upwind Multigrid Multi-Block Three-Dimensional Thin Layer Navier-Stokes Solver.

Degree: PhD, Mechanical & Aerospace Engineering, 1992, Old Dominion University

  A state-of-the-art computer code has been developed that incorporates a modified Runge-Kutta time integration scheme, Upwind numerical techniques, Multigrid acceleration, and Multi-block capabilities (RUMM).… (more)

Subjects/Keywords: Multiblock; Multigrid acceleration; Time integration; Turbulence; Upwind numerical techniques; Mechanical Engineering

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APA (6th Edition):

Cannizzaro, F. E. (1992). Runge-Kutta Upwind Multigrid Multi-Block Three-Dimensional Thin Layer Navier-Stokes Solver. (Doctoral Dissertation). Old Dominion University. Retrieved from https://digitalcommons.odu.edu/mae_etds/228

Chicago Manual of Style (16th Edition):

Cannizzaro, Frank E. “Runge-Kutta Upwind Multigrid Multi-Block Three-Dimensional Thin Layer Navier-Stokes Solver.” 1992. Doctoral Dissertation, Old Dominion University. Accessed December 05, 2020. https://digitalcommons.odu.edu/mae_etds/228.

MLA Handbook (7th Edition):

Cannizzaro, Frank E. “Runge-Kutta Upwind Multigrid Multi-Block Three-Dimensional Thin Layer Navier-Stokes Solver.” 1992. Web. 05 Dec 2020.

Vancouver:

Cannizzaro FE. Runge-Kutta Upwind Multigrid Multi-Block Three-Dimensional Thin Layer Navier-Stokes Solver. [Internet] [Doctoral dissertation]. Old Dominion University; 1992. [cited 2020 Dec 05]. Available from: https://digitalcommons.odu.edu/mae_etds/228.

Council of Science Editors:

Cannizzaro FE. Runge-Kutta Upwind Multigrid Multi-Block Three-Dimensional Thin Layer Navier-Stokes Solver. [Doctoral Dissertation]. Old Dominion University; 1992. Available from: https://digitalcommons.odu.edu/mae_etds/228

21. Gray, Carl E., Jr. Large-Amplitude Finite Element Flutter Analysis of Composite Panels in Hypersonic Flow.

Degree: PhD, Mechanical & Aerospace Engineering, 1991, Old Dominion University

  A finite-element approach is presented for determining the nonlinear flutter characteristics of two-dimensional isotropic and three-dimensional composite laminated thin panels using the third-order-piston, transverse… (more)

Subjects/Keywords: Composite panel; Flutter analysis; Hypersonic flow; Finite element; Applied Mechanics

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APA (6th Edition):

Gray, Carl E., J. (1991). Large-Amplitude Finite Element Flutter Analysis of Composite Panels in Hypersonic Flow. (Doctoral Dissertation). Old Dominion University. Retrieved from https://digitalcommons.odu.edu/mae_etds/232

Chicago Manual of Style (16th Edition):

Gray, Carl E., Jr. “Large-Amplitude Finite Element Flutter Analysis of Composite Panels in Hypersonic Flow.” 1991. Doctoral Dissertation, Old Dominion University. Accessed December 05, 2020. https://digitalcommons.odu.edu/mae_etds/232.

MLA Handbook (7th Edition):

Gray, Carl E., Jr. “Large-Amplitude Finite Element Flutter Analysis of Composite Panels in Hypersonic Flow.” 1991. Web. 05 Dec 2020.

Vancouver:

Gray, Carl E. J. Large-Amplitude Finite Element Flutter Analysis of Composite Panels in Hypersonic Flow. [Internet] [Doctoral dissertation]. Old Dominion University; 1991. [cited 2020 Dec 05]. Available from: https://digitalcommons.odu.edu/mae_etds/232.

Council of Science Editors:

Gray, Carl E. J. Large-Amplitude Finite Element Flutter Analysis of Composite Panels in Hypersonic Flow. [Doctoral Dissertation]. Old Dominion University; 1991. Available from: https://digitalcommons.odu.edu/mae_etds/232

22. Fouladi-Semnani, Kamran. Navier-Stokes Simulations of Flows About Complex Configurations Using Domain Decomposition Techniques.

Degree: PhD, Mechanical & Aerospace Engineering, 1990, Old Dominion University

  An algorithm is developed to obtain numerical simulations of flows about complex configurations composed of multiple and nonsimilar components with arbitrary geometries. The algorithm… (more)

Subjects/Keywords: Complex configuration; Navier-Stokes equations; Mechanical Engineering; Structures and Materials

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APA (6th Edition):

Fouladi-Semnani, K. (1990). Navier-Stokes Simulations of Flows About Complex Configurations Using Domain Decomposition Techniques. (Doctoral Dissertation). Old Dominion University. Retrieved from https://digitalcommons.odu.edu/mae_etds/234

Chicago Manual of Style (16th Edition):

Fouladi-Semnani, Kamran. “Navier-Stokes Simulations of Flows About Complex Configurations Using Domain Decomposition Techniques.” 1990. Doctoral Dissertation, Old Dominion University. Accessed December 05, 2020. https://digitalcommons.odu.edu/mae_etds/234.

MLA Handbook (7th Edition):

Fouladi-Semnani, Kamran. “Navier-Stokes Simulations of Flows About Complex Configurations Using Domain Decomposition Techniques.” 1990. Web. 05 Dec 2020.

Vancouver:

Fouladi-Semnani K. Navier-Stokes Simulations of Flows About Complex Configurations Using Domain Decomposition Techniques. [Internet] [Doctoral dissertation]. Old Dominion University; 1990. [cited 2020 Dec 05]. Available from: https://digitalcommons.odu.edu/mae_etds/234.

Council of Science Editors:

Fouladi-Semnani K. Navier-Stokes Simulations of Flows About Complex Configurations Using Domain Decomposition Techniques. [Doctoral Dissertation]. Old Dominion University; 1990. Available from: https://digitalcommons.odu.edu/mae_etds/234

23. Kandil, Hamdy A. Navier-Stokes Simulation of Quasi-Axisymmetric and Three-Dimensional Supersonic Vortex Breakdown.

Degree: PhD, Mechanical & Aerospace Engineering, 1993, Old Dominion University

  Computational simulation of supersonic vortex breakdown is considered for internal and external flow applications. The interaction of a supersonic swirling flow with a shock… (more)

Subjects/Keywords: Quasi axisymmetric flows; Navier-Stokes equations; Supersonic vortex breakdown; Mechanical Engineering; Structures and Materials

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APA (6th Edition):

Kandil, H. A. (1993). Navier-Stokes Simulation of Quasi-Axisymmetric and Three-Dimensional Supersonic Vortex Breakdown. (Doctoral Dissertation). Old Dominion University. Retrieved from https://digitalcommons.odu.edu/mae_etds/247

Chicago Manual of Style (16th Edition):

Kandil, Hamdy A. “Navier-Stokes Simulation of Quasi-Axisymmetric and Three-Dimensional Supersonic Vortex Breakdown.” 1993. Doctoral Dissertation, Old Dominion University. Accessed December 05, 2020. https://digitalcommons.odu.edu/mae_etds/247.

MLA Handbook (7th Edition):

Kandil, Hamdy A. “Navier-Stokes Simulation of Quasi-Axisymmetric and Three-Dimensional Supersonic Vortex Breakdown.” 1993. Web. 05 Dec 2020.

Vancouver:

Kandil HA. Navier-Stokes Simulation of Quasi-Axisymmetric and Three-Dimensional Supersonic Vortex Breakdown. [Internet] [Doctoral dissertation]. Old Dominion University; 1993. [cited 2020 Dec 05]. Available from: https://digitalcommons.odu.edu/mae_etds/247.

Council of Science Editors:

Kandil HA. Navier-Stokes Simulation of Quasi-Axisymmetric and Three-Dimensional Supersonic Vortex Breakdown. [Doctoral Dissertation]. Old Dominion University; 1993. Available from: https://digitalcommons.odu.edu/mae_etds/247

24. Hu, Hong. Full-Potential Integral Solutions for Steady and Unsteady Transonic Airfoils With and Without Embedded Euler Domains.

Degree: PhD, Mechanical & Aerospace Engineering, 1988, Old Dominion University

  The integral equation solution of the full-potential equation is presented for steady and unsteady transonic airfoil flow problems. The method is also coupled with… (more)

Subjects/Keywords: Integral equation solutions; Euler domains; Transonic airfoils; Transonic flows; Aerospace Engineering

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APA (6th Edition):

Hu, H. (1988). Full-Potential Integral Solutions for Steady and Unsteady Transonic Airfoils With and Without Embedded Euler Domains. (Doctoral Dissertation). Old Dominion University. Retrieved from https://digitalcommons.odu.edu/mae_etds/250

Chicago Manual of Style (16th Edition):

Hu, Hong. “Full-Potential Integral Solutions for Steady and Unsteady Transonic Airfoils With and Without Embedded Euler Domains.” 1988. Doctoral Dissertation, Old Dominion University. Accessed December 05, 2020. https://digitalcommons.odu.edu/mae_etds/250.

MLA Handbook (7th Edition):

Hu, Hong. “Full-Potential Integral Solutions for Steady and Unsteady Transonic Airfoils With and Without Embedded Euler Domains.” 1988. Web. 05 Dec 2020.

Vancouver:

Hu H. Full-Potential Integral Solutions for Steady and Unsteady Transonic Airfoils With and Without Embedded Euler Domains. [Internet] [Doctoral dissertation]. Old Dominion University; 1988. [cited 2020 Dec 05]. Available from: https://digitalcommons.odu.edu/mae_etds/250.

Council of Science Editors:

Hu H. Full-Potential Integral Solutions for Steady and Unsteady Transonic Airfoils With and Without Embedded Euler Domains. [Doctoral Dissertation]. Old Dominion University; 1988. Available from: https://digitalcommons.odu.edu/mae_etds/250

25. Abdelhamid, Yahia A. Large Amplitude Pitching of Supermaneuver Delta Wings Including Flow Control.

Degree: PhD, Aerospace Engineering, 1999, Old Dominion University

  The unsteady, three-dimensional Navier-Stokes equations are solved to simulate and study the aerodynamic response of a delta wing undergoing large amplitude pitching motion up… (more)

Subjects/Keywords: Aerodynamic response; Delta wings; Flow control; Pitching; Aerodynamics and Fluid Mechanics; Engineering Mechanics; Structures and Materials

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APA (6th Edition):

Abdelhamid, Y. A. (1999). Large Amplitude Pitching of Supermaneuver Delta Wings Including Flow Control. (Doctoral Dissertation). Old Dominion University. Retrieved from 9780599524989 ; https://digitalcommons.odu.edu/mae_etds/52

Chicago Manual of Style (16th Edition):

Abdelhamid, Yahia A. “Large Amplitude Pitching of Supermaneuver Delta Wings Including Flow Control.” 1999. Doctoral Dissertation, Old Dominion University. Accessed December 05, 2020. 9780599524989 ; https://digitalcommons.odu.edu/mae_etds/52.

MLA Handbook (7th Edition):

Abdelhamid, Yahia A. “Large Amplitude Pitching of Supermaneuver Delta Wings Including Flow Control.” 1999. Web. 05 Dec 2020.

Vancouver:

Abdelhamid YA. Large Amplitude Pitching of Supermaneuver Delta Wings Including Flow Control. [Internet] [Doctoral dissertation]. Old Dominion University; 1999. [cited 2020 Dec 05]. Available from: 9780599524989 ; https://digitalcommons.odu.edu/mae_etds/52.

Council of Science Editors:

Abdelhamid YA. Large Amplitude Pitching of Supermaneuver Delta Wings Including Flow Control. [Doctoral Dissertation]. Old Dominion University; 1999. Available from: 9780599524989 ; https://digitalcommons.odu.edu/mae_etds/52

26. Elshabasy, Mohamed Mostafa Yousef Bassyouny. Mitigating Crack Propagation in a Highly Maneuverable Flight Vehicle Using Life Extending Control Logic.

Degree: PhD, Aerospace Engineering, 2009, Old Dominion University

  In this research, life extending control logic is proposed to reduce the cost of treating the aging problem of military aircraft structures and to… (more)

Subjects/Keywords: Control; Crack; Crack propagation; Flight; Flight vehicle; Life; Life-extending control logic; Mitigating; Propagation; Aerospace Engineering

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APA (6th Edition):

Elshabasy, M. M. Y. B. (2009). Mitigating Crack Propagation in a Highly Maneuverable Flight Vehicle Using Life Extending Control Logic. (Doctoral Dissertation). Old Dominion University. Retrieved from 9781109284447 ; https://digitalcommons.odu.edu/mae_etds/55

Chicago Manual of Style (16th Edition):

Elshabasy, Mohamed Mostafa Yousef Bassyouny. “Mitigating Crack Propagation in a Highly Maneuverable Flight Vehicle Using Life Extending Control Logic.” 2009. Doctoral Dissertation, Old Dominion University. Accessed December 05, 2020. 9781109284447 ; https://digitalcommons.odu.edu/mae_etds/55.

MLA Handbook (7th Edition):

Elshabasy, Mohamed Mostafa Yousef Bassyouny. “Mitigating Crack Propagation in a Highly Maneuverable Flight Vehicle Using Life Extending Control Logic.” 2009. Web. 05 Dec 2020.

Vancouver:

Elshabasy MMYB. Mitigating Crack Propagation in a Highly Maneuverable Flight Vehicle Using Life Extending Control Logic. [Internet] [Doctoral dissertation]. Old Dominion University; 2009. [cited 2020 Dec 05]. Available from: 9781109284447 ; https://digitalcommons.odu.edu/mae_etds/55.

Council of Science Editors:

Elshabasy MMYB. Mitigating Crack Propagation in a Highly Maneuverable Flight Vehicle Using Life Extending Control Logic. [Doctoral Dissertation]. Old Dominion University; 2009. Available from: 9781109284447 ; https://digitalcommons.odu.edu/mae_etds/55

27. Menzies, Margaret Anne. Unsteady, Transonic Flow Around Delta Wings Undergoing Coupled and Natural Modes Response: A Multidisciplinary Problem.

Degree: PhD, Aerospace Engineering, 1996, Old Dominion University

  The unsteady, three-dimensional Navier-Stokes equations coupled with the Euler equations of rigid-body dynamics are sequentially solved to simulate and analyze the aerodynamic response of… (more)

Subjects/Keywords: Delta wings; Transonic flow; Modes response; Aerospace Engineering; Mechanical Engineering; Structures and Materials

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APA (6th Edition):

Menzies, M. A. (1996). Unsteady, Transonic Flow Around Delta Wings Undergoing Coupled and Natural Modes Response: A Multidisciplinary Problem. (Doctoral Dissertation). Old Dominion University. Retrieved from https://digitalcommons.odu.edu/mae_etds/75

Chicago Manual of Style (16th Edition):

Menzies, Margaret Anne. “Unsteady, Transonic Flow Around Delta Wings Undergoing Coupled and Natural Modes Response: A Multidisciplinary Problem.” 1996. Doctoral Dissertation, Old Dominion University. Accessed December 05, 2020. https://digitalcommons.odu.edu/mae_etds/75.

MLA Handbook (7th Edition):

Menzies, Margaret Anne. “Unsteady, Transonic Flow Around Delta Wings Undergoing Coupled and Natural Modes Response: A Multidisciplinary Problem.” 1996. Web. 05 Dec 2020.

Vancouver:

Menzies MA. Unsteady, Transonic Flow Around Delta Wings Undergoing Coupled and Natural Modes Response: A Multidisciplinary Problem. [Internet] [Doctoral dissertation]. Old Dominion University; 1996. [cited 2020 Dec 05]. Available from: https://digitalcommons.odu.edu/mae_etds/75.

Council of Science Editors:

Menzies MA. Unsteady, Transonic Flow Around Delta Wings Undergoing Coupled and Natural Modes Response: A Multidisciplinary Problem. [Doctoral Dissertation]. Old Dominion University; 1996. Available from: https://digitalcommons.odu.edu/mae_etds/75

28. Massey, Steven J. Development of a Coupled Fluid/Structure Aeroelastic Solver with Applications to Vortex Breakdown-Induced Twin Tail Buffeting.

Degree: PhD, Aerospace Engineering, 2007, Old Dominion University

  Simulation of tail buffet is studied for several delta wing-vertical tail configurations. Flow conditions are chosen such that the wing primary-vortex cores experience vortex… (more)

Subjects/Keywords: Elastic deformation; Flow; Grid displacements; Aerospace Engineering; Structures and Materials

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APA (6th Edition):

Massey, S. J. (2007). Development of a Coupled Fluid/Structure Aeroelastic Solver with Applications to Vortex Breakdown-Induced Twin Tail Buffeting. (Doctoral Dissertation). Old Dominion University. Retrieved from 9780591623383 ; https://digitalcommons.odu.edu/mae_etds/76

Chicago Manual of Style (16th Edition):

Massey, Steven J. “Development of a Coupled Fluid/Structure Aeroelastic Solver with Applications to Vortex Breakdown-Induced Twin Tail Buffeting.” 2007. Doctoral Dissertation, Old Dominion University. Accessed December 05, 2020. 9780591623383 ; https://digitalcommons.odu.edu/mae_etds/76.

MLA Handbook (7th Edition):

Massey, Steven J. “Development of a Coupled Fluid/Structure Aeroelastic Solver with Applications to Vortex Breakdown-Induced Twin Tail Buffeting.” 2007. Web. 05 Dec 2020.

Vancouver:

Massey SJ. Development of a Coupled Fluid/Structure Aeroelastic Solver with Applications to Vortex Breakdown-Induced Twin Tail Buffeting. [Internet] [Doctoral dissertation]. Old Dominion University; 2007. [cited 2020 Dec 05]. Available from: 9780591623383 ; https://digitalcommons.odu.edu/mae_etds/76.

Council of Science Editors:

Massey SJ. Development of a Coupled Fluid/Structure Aeroelastic Solver with Applications to Vortex Breakdown-Induced Twin Tail Buffeting. [Doctoral Dissertation]. Old Dominion University; 2007. Available from: 9780591623383 ; https://digitalcommons.odu.edu/mae_etds/76

29. Ozcer, Isik A. Multidisciplinary Design Optimization for Sonic Boom Mitigation.

Degree: PhD, Aerospace Engineering, 2009, Old Dominion University

  Automated, parallelized, time-efficient surface definition and grid generation and flow simulation methods are developed for sharp and accurate sonic boom signal computation in three… (more)

Subjects/Keywords: Sonic boom; Supersonic flow; Unstructured Grid Adaptation; Aerospace Engineering

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APA (6th Edition):

Ozcer, I. A. (2009). Multidisciplinary Design Optimization for Sonic Boom Mitigation. (Doctoral Dissertation). Old Dominion University. Retrieved from 9781109142815 ; https://digitalcommons.odu.edu/mae_etds/79

Chicago Manual of Style (16th Edition):

Ozcer, Isik A. “Multidisciplinary Design Optimization for Sonic Boom Mitigation.” 2009. Doctoral Dissertation, Old Dominion University. Accessed December 05, 2020. 9781109142815 ; https://digitalcommons.odu.edu/mae_etds/79.

MLA Handbook (7th Edition):

Ozcer, Isik A. “Multidisciplinary Design Optimization for Sonic Boom Mitigation.” 2009. Web. 05 Dec 2020.

Vancouver:

Ozcer IA. Multidisciplinary Design Optimization for Sonic Boom Mitigation. [Internet] [Doctoral dissertation]. Old Dominion University; 2009. [cited 2020 Dec 05]. Available from: 9781109142815 ; https://digitalcommons.odu.edu/mae_etds/79.

Council of Science Editors:

Ozcer IA. Multidisciplinary Design Optimization for Sonic Boom Mitigation. [Doctoral Dissertation]. Old Dominion University; 2009. Available from: 9781109142815 ; https://digitalcommons.odu.edu/mae_etds/79

30. Palaez, Juan A. Implementation and Testing of Unsteady Reynolds-Averaged Navier-Stokes and Detached Eddy Simulation Using an Implicit Unstructured Multigrid Scheme.

Degree: PhD, Aerospace Engineering, 2003, Old Dominion University

  Investigation and development of the Detached Eddy Simulation (DES) technique for the computation of unsteady flows on unstructured grids are presented. The motivation of… (more)

Subjects/Keywords: Agglomeration; Computational fluid dynamics; Eddy simulation; Multigrid; Reynolds-averaged Navier-Stokes; Aerodynamics and Fluid Mechanics; Aerospace Engineering; Structures and Materials

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APA (6th Edition):

Palaez, J. A. (2003). Implementation and Testing of Unsteady Reynolds-Averaged Navier-Stokes and Detached Eddy Simulation Using an Implicit Unstructured Multigrid Scheme. (Doctoral Dissertation). Old Dominion University. Retrieved from https://digitalcommons.odu.edu/mae_etds/84

Chicago Manual of Style (16th Edition):

Palaez, Juan A. “Implementation and Testing of Unsteady Reynolds-Averaged Navier-Stokes and Detached Eddy Simulation Using an Implicit Unstructured Multigrid Scheme.” 2003. Doctoral Dissertation, Old Dominion University. Accessed December 05, 2020. https://digitalcommons.odu.edu/mae_etds/84.

MLA Handbook (7th Edition):

Palaez, Juan A. “Implementation and Testing of Unsteady Reynolds-Averaged Navier-Stokes and Detached Eddy Simulation Using an Implicit Unstructured Multigrid Scheme.” 2003. Web. 05 Dec 2020.

Vancouver:

Palaez JA. Implementation and Testing of Unsteady Reynolds-Averaged Navier-Stokes and Detached Eddy Simulation Using an Implicit Unstructured Multigrid Scheme. [Internet] [Doctoral dissertation]. Old Dominion University; 2003. [cited 2020 Dec 05]. Available from: https://digitalcommons.odu.edu/mae_etds/84.

Council of Science Editors:

Palaez JA. Implementation and Testing of Unsteady Reynolds-Averaged Navier-Stokes and Detached Eddy Simulation Using an Implicit Unstructured Multigrid Scheme. [Doctoral Dissertation]. Old Dominion University; 2003. Available from: https://digitalcommons.odu.edu/mae_etds/84

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