Advanced search options

Sorted by: relevance · author · university · date | New search

You searched for `+publisher:"Old Dominion University" +contributor:("Osama A. Kandil")`

.
Showing records 1 – 30 of
31 total matches.

Search Limiters

Department

▼ Search Limiters

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

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

URL: 9780542855351 ; https://digitalcommons.odu.edu/mae_etds/54

► 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

Record Details Similar Records

❌

APA · Chicago · MLA · Vancouver · CSE | Export to Zotero / EndNote / Reference Manager

APA (6^{th} 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 (16^{th} 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 (7^{th} 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

URL: 9780542189166 ; https://digitalcommons.odu.edu/mae_etds/184

► 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

Record Details Similar Records

❌

APA · Chicago · MLA · Vancouver · CSE | Export to Zotero / EndNote / Reference Manager

APA (6^{th} 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 (16^{th} 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 (7^{th} 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

URL: 9780493712970 ; https://digitalcommons.odu.edu/mae_etds/49

► 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

Record Details Similar Records

❌

APA · Chicago · MLA · Vancouver · CSE | Export to Zotero / EndNote / Reference Manager

APA (6^{th} 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 (16^{th} 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 (7^{th} 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

URL: 9781109566369 ; https://digitalcommons.odu.edu/mae_etds/53

► 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

Record Details Similar Records

❌

APA · Chicago · MLA · Vancouver · CSE | Export to Zotero / EndNote / Reference Manager

APA (6^{th} 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 (16^{th} 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 (7^{th} 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

URL: 9780549928584 ; https://digitalcommons.odu.edu/mae_etds/64

► 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

Record Details Similar Records

❌

APA · Chicago · MLA · Vancouver · CSE | Export to Zotero / EndNote / Reference Manager

APA (6^{th} 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 (16^{th} 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 (7^{th} 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

URL: 9780549069454 ; https://digitalcommons.odu.edu/mae_etds/70

► 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

Record Details Similar Records

❌

APA · Chicago · MLA · Vancouver · CSE | Export to Zotero / EndNote / Reference Manager

APA (6^{th} 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 (16^{th} 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 (7^{th} 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

URL: 9780549329459 ; https://digitalcommons.odu.edu/mae_etds/72

► 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

Record Details Similar Records

❌

APA · Chicago · MLA · Vancouver · CSE | Export to Zotero / EndNote / Reference Manager

APA (6^{th} 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 (16^{th} 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 (7^{th} 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

URL: 9780542753879 ; https://digitalcommons.odu.edu/mae_etds/74

► 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

Record Details Similar Records

❌

APA · Chicago · MLA · Vancouver · CSE | Export to Zotero / EndNote / Reference Manager

APA (6^{th} 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 (16^{th} 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 (7^{th} 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

URL: 9780599525108 ; https://digitalcommons.odu.edu/mae_etds/80

► 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

Record Details Similar Records

❌

APA · Chicago · MLA · Vancouver · CSE | Export to Zotero / EndNote / Reference Manager

APA (6^{th} 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 (16^{th} 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 (7^{th} 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

URL: 9781124504278 ; https://digitalcommons.odu.edu/mae_etds/92

► 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

Record Details Similar Records

❌

APA · Chicago · MLA · Vancouver · CSE | Export to Zotero / EndNote / Reference Manager

APA (6^{th} 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 (16^{th} 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 (7^{th} 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

URL: 9780493976112 ; https://digitalcommons.odu.edu/mae_etds/94

► 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

Record Details Similar Records

❌

APA · Chicago · MLA · Vancouver · CSE | Export to Zotero / EndNote / Reference Manager

APA (6^{th} 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 (16^{th} 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 (7^{th} 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

URL: https://digitalcommons.odu.edu/mae_etds/96

► 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

Record Details Similar Records

❌

APA · Chicago · MLA · Vancouver · CSE | Export to Zotero / EndNote / Reference Manager

APA (6^{th} 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 (16^{th} 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 (7^{th} 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

URL: https://digitalcommons.odu.edu/mae_etds/267

► 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

Record Details Similar Records

❌

APA · Chicago · MLA · Vancouver · CSE | Export to Zotero / EndNote / Reference Manager

APA (6^{th} 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 (16^{th} 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 (7^{th} 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

URL: https://digitalcommons.odu.edu/mae_etds/268

► 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

Record Details Similar Records

❌

APA · Chicago · MLA · Vancouver · CSE | Export to Zotero / EndNote / Reference Manager

APA (6^{th} 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 (16^{th} 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 (7^{th} 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

URL: https://digitalcommons.odu.edu/mae_etds/291

► 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

Record Details Similar Records

❌

APA · Chicago · MLA · Vancouver · CSE | Export to Zotero / EndNote / Reference Manager

APA (6^{th} 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 (16^{th} 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 (7^{th} 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

URL: https://digitalcommons.odu.edu/mae_etds/296

► 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

Record Details Similar Records

❌

APA · Chicago · MLA · Vancouver · CSE | Export to Zotero / EndNote / Reference Manager

APA (6^{th} 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 (16^{th} 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 (7^{th} 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

URL: https://digitalcommons.odu.edu/mae_etds/297

► 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

Record Details Similar Records

❌

APA · Chicago · MLA · Vancouver · CSE | Export to Zotero / EndNote / Reference Manager

APA (6^{th} 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 (16^{th} 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 (7^{th} 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

URL: 9780493177960 ; https://digitalcommons.odu.edu/mae_etds/192

► 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

Record Details Similar Records

❌

APA · Chicago · MLA · Vancouver · CSE | Export to Zotero / EndNote / Reference Manager

APA (6^{th} 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 (16^{th} 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 (7^{th} 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

URL: https://digitalcommons.odu.edu/mae_etds/222

► 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

Record Details Similar Records

❌

APA · Chicago · MLA · Vancouver · CSE | Export to Zotero / EndNote / Reference Manager

APA (6^{th} 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 (16^{th} 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 (7^{th} 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

URL: https://digitalcommons.odu.edu/mae_etds/228

► 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

Record Details Similar Records

❌

APA · Chicago · MLA · Vancouver · CSE | Export to Zotero / EndNote / Reference Manager

APA (6^{th} 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 (16^{th} 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 (7^{th} 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

URL: https://digitalcommons.odu.edu/mae_etds/232

► 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

Record Details Similar Records

❌

APA · Chicago · MLA · Vancouver · CSE | Export to Zotero / EndNote / Reference Manager

APA (6^{th} 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 (16^{th} 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 (7^{th} 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

URL: https://digitalcommons.odu.edu/mae_etds/234

► 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

Record Details Similar Records

❌

APA · Chicago · MLA · Vancouver · CSE | Export to Zotero / EndNote / Reference Manager

APA (6^{th} 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 (16^{th} 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 (7^{th} 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

URL: https://digitalcommons.odu.edu/mae_etds/247

► 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

Record Details Similar Records

❌

APA · Chicago · MLA · Vancouver · CSE | Export to Zotero / EndNote / Reference Manager

APA (6^{th} 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 (16^{th} 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 (7^{th} 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

URL: https://digitalcommons.odu.edu/mae_etds/250

► 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

Record Details Similar Records

❌

APA · Chicago · MLA · Vancouver · CSE | Export to Zotero / EndNote / Reference Manager

APA (6^{th} 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 (16^{th} 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 (7^{th} 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

URL: 9780599524989 ; https://digitalcommons.odu.edu/mae_etds/52

► 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

Record Details Similar Records

❌

APA · Chicago · MLA · Vancouver · CSE | Export to Zotero / EndNote / Reference Manager

APA (6^{th} 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 (16^{th} 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 (7^{th} 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

URL: 9781109284447 ; https://digitalcommons.odu.edu/mae_etds/55

► 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

Record Details Similar Records

❌

APA · Chicago · MLA · Vancouver · CSE | Export to Zotero / EndNote / Reference Manager

APA (6^{th} 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 (16^{th} 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 (7^{th} 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

URL: https://digitalcommons.odu.edu/mae_etds/75

► 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

Record Details Similar Records

❌

APA · Chicago · MLA · Vancouver · CSE | Export to Zotero / EndNote / Reference Manager

APA (6^{th} 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 (16^{th} 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 (7^{th} 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

URL: 9780591623383 ; https://digitalcommons.odu.edu/mae_etds/76

► 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

Record Details Similar Records

❌

APA · Chicago · MLA · Vancouver · CSE | Export to Zotero / EndNote / Reference Manager

APA (6^{th} 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 (16^{th} 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 (7^{th} 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

URL: 9781109142815 ; https://digitalcommons.odu.edu/mae_etds/79

► 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

Record Details Similar Records

❌

APA · Chicago · MLA · Vancouver · CSE | Export to Zotero / EndNote / Reference Manager

APA (6^{th} 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 (16^{th} 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 (7^{th} 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

URL: https://digitalcommons.odu.edu/mae_etds/84

► 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

Record Details Similar Records

❌

APA · Chicago · MLA · Vancouver · CSE | Export to Zotero / EndNote / Reference Manager

APA (6^{th} 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 (16^{th} 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 (7^{th} 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