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You searched for +publisher:"Virginia Tech" +contributor:("Mason, William H."). Showing records 1 – 30 of 110 total matches.

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Virginia Tech

1. Friedman, Alex Matthew. An Approach to Incorporate Additive Manufacturing and Rapid Prototype Testing for Aircraft Conceptual Design to Improve MDO Effectiveness.

Degree: MS, Aerospace Engineering, 2015, Virginia Tech

 The primary objectives of this work are two-fold. First, additive manufacturing (AM) and rapid prototype (RP) testing are evaluated for use in production of a… (more)

Subjects/Keywords: Additive Manufacturing; Surrogate-Based Optimization; Aircraft Conceptual Design Effectiveness; Design of Experiments

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APA (6th Edition):

Friedman, A. M. (2015). An Approach to Incorporate Additive Manufacturing and Rapid Prototype Testing for Aircraft Conceptual Design to Improve MDO Effectiveness. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/73656

Chicago Manual of Style (16th Edition):

Friedman, Alex Matthew. “An Approach to Incorporate Additive Manufacturing and Rapid Prototype Testing for Aircraft Conceptual Design to Improve MDO Effectiveness.” 2015. Masters Thesis, Virginia Tech. Accessed January 20, 2021. http://hdl.handle.net/10919/73656.

MLA Handbook (7th Edition):

Friedman, Alex Matthew. “An Approach to Incorporate Additive Manufacturing and Rapid Prototype Testing for Aircraft Conceptual Design to Improve MDO Effectiveness.” 2015. Web. 20 Jan 2021.

Vancouver:

Friedman AM. An Approach to Incorporate Additive Manufacturing and Rapid Prototype Testing for Aircraft Conceptual Design to Improve MDO Effectiveness. [Internet] [Masters thesis]. Virginia Tech; 2015. [cited 2021 Jan 20]. Available from: http://hdl.handle.net/10919/73656.

Council of Science Editors:

Friedman AM. An Approach to Incorporate Additive Manufacturing and Rapid Prototype Testing for Aircraft Conceptual Design to Improve MDO Effectiveness. [Masters Thesis]. Virginia Tech; 2015. Available from: http://hdl.handle.net/10919/73656


Virginia Tech

2. Knight, Kyle Cohn Davis. Assessment of RANS Turbulence Models for Strut-Wing Junctions.

Degree: MS, Aerospace Engineering, 2011, Virginia Tech

 Multidisciplinary Design Optimization (MDO) studies show the Strut/Truss Braced Wing (SBW/TBW) concept has the potential to save a significant amount of fuel over conventional designs.… (more)

Subjects/Keywords: Turbulence; Interference; Transonic

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APA (6th Edition):

Knight, K. C. D. (2011). Assessment of RANS Turbulence Models for Strut-Wing Junctions. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/31760

Chicago Manual of Style (16th Edition):

Knight, Kyle Cohn Davis. “Assessment of RANS Turbulence Models for Strut-Wing Junctions.” 2011. Masters Thesis, Virginia Tech. Accessed January 20, 2021. http://hdl.handle.net/10919/31760.

MLA Handbook (7th Edition):

Knight, Kyle Cohn Davis. “Assessment of RANS Turbulence Models for Strut-Wing Junctions.” 2011. Web. 20 Jan 2021.

Vancouver:

Knight KCD. Assessment of RANS Turbulence Models for Strut-Wing Junctions. [Internet] [Masters thesis]. Virginia Tech; 2011. [cited 2021 Jan 20]. Available from: http://hdl.handle.net/10919/31760.

Council of Science Editors:

Knight KCD. Assessment of RANS Turbulence Models for Strut-Wing Junctions. [Masters Thesis]. Virginia Tech; 2011. Available from: http://hdl.handle.net/10919/31760


Virginia Tech

3. Phillips, Tyrone. Extrapolation-based Discretization Error and Uncertainty Estimation in Computational Fluid Dynamics.

Degree: MS, Aerospace and Ocean Engineering, 2012, Virginia Tech

 The solution to partial differential equations generally requires approximations that result in numerical error in the final solution. Of the different types of numerical error… (more)

Subjects/Keywords: Richardson Extrapolation; Navier-Stokes; Grid Convergence Index; Finite Volume Method; Euler

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APA (6th Edition):

Phillips, T. (2012). Extrapolation-based Discretization Error and Uncertainty Estimation in Computational Fluid Dynamics. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/31504

Chicago Manual of Style (16th Edition):

Phillips, Tyrone. “Extrapolation-based Discretization Error and Uncertainty Estimation in Computational Fluid Dynamics.” 2012. Masters Thesis, Virginia Tech. Accessed January 20, 2021. http://hdl.handle.net/10919/31504.

MLA Handbook (7th Edition):

Phillips, Tyrone. “Extrapolation-based Discretization Error and Uncertainty Estimation in Computational Fluid Dynamics.” 2012. Web. 20 Jan 2021.

Vancouver:

Phillips T. Extrapolation-based Discretization Error and Uncertainty Estimation in Computational Fluid Dynamics. [Internet] [Masters thesis]. Virginia Tech; 2012. [cited 2021 Jan 20]. Available from: http://hdl.handle.net/10919/31504.

Council of Science Editors:

Phillips T. Extrapolation-based Discretization Error and Uncertainty Estimation in Computational Fluid Dynamics. [Masters Thesis]. Virginia Tech; 2012. Available from: http://hdl.handle.net/10919/31504


Virginia Tech

4. Ghoman, Satyajit Sudhir. A Hybrid Optimization Framework with POD-based Order Reduction and Design-Space Evolution Scheme.

Degree: PhD, Aerospace Engineering, 2013, Virginia Tech

 The main objective of this research is to develop an innovative multi-fidelity multi-disciplinary design, analysis and optimization suite that integrates certain solution generation codes and… (more)

Subjects/Keywords: Multi-disciplinary Optimization; Proper Orthogonal Decomposition; Evolutionary Algorithm; Aeroelasticity

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APA (6th Edition):

Ghoman, S. S. (2013). A Hybrid Optimization Framework with POD-based Order Reduction and Design-Space Evolution Scheme. (Doctoral Dissertation). Virginia Tech. Retrieved from http://hdl.handle.net/10919/23113

Chicago Manual of Style (16th Edition):

Ghoman, Satyajit Sudhir. “A Hybrid Optimization Framework with POD-based Order Reduction and Design-Space Evolution Scheme.” 2013. Doctoral Dissertation, Virginia Tech. Accessed January 20, 2021. http://hdl.handle.net/10919/23113.

MLA Handbook (7th Edition):

Ghoman, Satyajit Sudhir. “A Hybrid Optimization Framework with POD-based Order Reduction and Design-Space Evolution Scheme.” 2013. Web. 20 Jan 2021.

Vancouver:

Ghoman SS. A Hybrid Optimization Framework with POD-based Order Reduction and Design-Space Evolution Scheme. [Internet] [Doctoral dissertation]. Virginia Tech; 2013. [cited 2021 Jan 20]. Available from: http://hdl.handle.net/10919/23113.

Council of Science Editors:

Ghoman SS. A Hybrid Optimization Framework with POD-based Order Reduction and Design-Space Evolution Scheme. [Doctoral Dissertation]. Virginia Tech; 2013. Available from: http://hdl.handle.net/10919/23113


Virginia Tech

5. Walker, William Paul. Optimization of Harmonically Deforming Thin Airfoils and Membrane Wings for Optimum Thrust and Efficiency.

Degree: PhD, Aerospace and Ocean Engineering, 2012, Virginia Tech

 This dissertation presents both analytical and numerical approaches to optimizing thrust and thrust efficiency of harmonically deforming thin airfoils and membrane wings. A frequency domain… (more)

Subjects/Keywords: Unsteady Aerodynamics; Deformable Airfoils; Membrane Aeroelasticity; Aeroelastic Tailoring; Optimization

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APA (6th Edition):

Walker, W. P. (2012). Optimization of Harmonically Deforming Thin Airfoils and Membrane Wings for Optimum Thrust and Efficiency. (Doctoral Dissertation). Virginia Tech. Retrieved from http://hdl.handle.net/10919/27748

Chicago Manual of Style (16th Edition):

Walker, William Paul. “Optimization of Harmonically Deforming Thin Airfoils and Membrane Wings for Optimum Thrust and Efficiency.” 2012. Doctoral Dissertation, Virginia Tech. Accessed January 20, 2021. http://hdl.handle.net/10919/27748.

MLA Handbook (7th Edition):

Walker, William Paul. “Optimization of Harmonically Deforming Thin Airfoils and Membrane Wings for Optimum Thrust and Efficiency.” 2012. Web. 20 Jan 2021.

Vancouver:

Walker WP. Optimization of Harmonically Deforming Thin Airfoils and Membrane Wings for Optimum Thrust and Efficiency. [Internet] [Doctoral dissertation]. Virginia Tech; 2012. [cited 2021 Jan 20]. Available from: http://hdl.handle.net/10919/27748.

Council of Science Editors:

Walker WP. Optimization of Harmonically Deforming Thin Airfoils and Membrane Wings for Optimum Thrust and Efficiency. [Doctoral Dissertation]. Virginia Tech; 2012. Available from: http://hdl.handle.net/10919/27748


Virginia Tech

6. Butler, William M. The Impact of Simulation-Based Learning in Aircraft Design on Aerospace Student Preparedness for Engineering Practice: A Mixed Methods Approach.

Degree: PhD, Engineering Education, 2012, Virginia Tech

 It has been said that engineers create that which never was. The university experience is a key component in preparing engineers who support the creation… (more)

Subjects/Keywords: aerospace; design; engineering education; simulation

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APA (6th Edition):

Butler, W. M. (2012). The Impact of Simulation-Based Learning in Aircraft Design on Aerospace Student Preparedness for Engineering Practice: A Mixed Methods Approach. (Doctoral Dissertation). Virginia Tech. Retrieved from http://hdl.handle.net/10919/27601

Chicago Manual of Style (16th Edition):

Butler, William M. “The Impact of Simulation-Based Learning in Aircraft Design on Aerospace Student Preparedness for Engineering Practice: A Mixed Methods Approach.” 2012. Doctoral Dissertation, Virginia Tech. Accessed January 20, 2021. http://hdl.handle.net/10919/27601.

MLA Handbook (7th Edition):

Butler, William M. “The Impact of Simulation-Based Learning in Aircraft Design on Aerospace Student Preparedness for Engineering Practice: A Mixed Methods Approach.” 2012. Web. 20 Jan 2021.

Vancouver:

Butler WM. The Impact of Simulation-Based Learning in Aircraft Design on Aerospace Student Preparedness for Engineering Practice: A Mixed Methods Approach. [Internet] [Doctoral dissertation]. Virginia Tech; 2012. [cited 2021 Jan 20]. Available from: http://hdl.handle.net/10919/27601.

Council of Science Editors:

Butler WM. The Impact of Simulation-Based Learning in Aircraft Design on Aerospace Student Preparedness for Engineering Practice: A Mixed Methods Approach. [Doctoral Dissertation]. Virginia Tech; 2012. Available from: http://hdl.handle.net/10919/27601


Virginia Tech

7. Freeman, Jacob Andrew. Optimization Under Uncertainty and Total Predictive Uncertainty for a Tractor-Trailer Base-Drag Reduction Device.

Degree: PhD, Aerospace and Ocean Engineering, 2012, Virginia Tech

 One key outcome of this research is the design for a 3-D tractor-trailer base-drag reduction device that predicts a 41% reduction in wind-averaged drag coefficient… (more)

Subjects/Keywords: aerodynamic shape optimization; optimization under uncertainty; predictive uncertainty; verification and validation; drag reduction; evolutionary algorithm; uncertainty quantification

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APA (6th Edition):

Freeman, J. A. (2012). Optimization Under Uncertainty and Total Predictive Uncertainty for a Tractor-Trailer Base-Drag Reduction Device. (Doctoral Dissertation). Virginia Tech. Retrieved from http://hdl.handle.net/10919/77168

Chicago Manual of Style (16th Edition):

Freeman, Jacob Andrew. “Optimization Under Uncertainty and Total Predictive Uncertainty for a Tractor-Trailer Base-Drag Reduction Device.” 2012. Doctoral Dissertation, Virginia Tech. Accessed January 20, 2021. http://hdl.handle.net/10919/77168.

MLA Handbook (7th Edition):

Freeman, Jacob Andrew. “Optimization Under Uncertainty and Total Predictive Uncertainty for a Tractor-Trailer Base-Drag Reduction Device.” 2012. Web. 20 Jan 2021.

Vancouver:

Freeman JA. Optimization Under Uncertainty and Total Predictive Uncertainty for a Tractor-Trailer Base-Drag Reduction Device. [Internet] [Doctoral dissertation]. Virginia Tech; 2012. [cited 2021 Jan 20]. Available from: http://hdl.handle.net/10919/77168.

Council of Science Editors:

Freeman JA. Optimization Under Uncertainty and Total Predictive Uncertainty for a Tractor-Trailer Base-Drag Reduction Device. [Doctoral Dissertation]. Virginia Tech; 2012. Available from: http://hdl.handle.net/10919/77168

8. Standridge, Zachary Dakotah. Design and Development of Low-cost Multi-function UAV Suitable for Production and Operation in Low Resource Environments.

Degree: MS, Aerospace Engineering, 2018, Virginia Tech

 A new flying wing design has been developed at the Unmanned Systems Lab (USL) at Virginia Tech to serve delivery and remote sensing applications in… (more)

Subjects/Keywords: Rapid Prototyping; Developing Country; Posterboard Wings; UAV Design; Range Optimization

…Lab at Virginia Tech is always looking out for potential UAV uses. To name a few: drones to… 

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APA (6th Edition):

Standridge, Z. D. (2018). Design and Development of Low-cost Multi-function UAV Suitable for Production and Operation in Low Resource Environments. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/83877

Chicago Manual of Style (16th Edition):

Standridge, Zachary Dakotah. “Design and Development of Low-cost Multi-function UAV Suitable for Production and Operation in Low Resource Environments.” 2018. Masters Thesis, Virginia Tech. Accessed January 20, 2021. http://hdl.handle.net/10919/83877.

MLA Handbook (7th Edition):

Standridge, Zachary Dakotah. “Design and Development of Low-cost Multi-function UAV Suitable for Production and Operation in Low Resource Environments.” 2018. Web. 20 Jan 2021.

Vancouver:

Standridge ZD. Design and Development of Low-cost Multi-function UAV Suitable for Production and Operation in Low Resource Environments. [Internet] [Masters thesis]. Virginia Tech; 2018. [cited 2021 Jan 20]. Available from: http://hdl.handle.net/10919/83877.

Council of Science Editors:

Standridge ZD. Design and Development of Low-cost Multi-function UAV Suitable for Production and Operation in Low Resource Environments. [Masters Thesis]. Virginia Tech; 2018. Available from: http://hdl.handle.net/10919/83877


Virginia Tech

9. Phillips, Tyrone. Residual-based Discretization Error Estimation for Computational Fluid Dynamics.

Degree: PhD, Aerospace Engineering, 2014, Virginia Tech

 The largest and most difficult numerical approximation error to estimate is discretization error. Residual-based discretization error estimation methods are a category of error estimators that… (more)

Subjects/Keywords: CFD; solution reconstruction; discretization error; truncation error; defect correction; error transport equations

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APA (6th Edition):

Phillips, T. (2014). Residual-based Discretization Error Estimation for Computational Fluid Dynamics. (Doctoral Dissertation). Virginia Tech. Retrieved from http://hdl.handle.net/10919/50647

Chicago Manual of Style (16th Edition):

Phillips, Tyrone. “Residual-based Discretization Error Estimation for Computational Fluid Dynamics.” 2014. Doctoral Dissertation, Virginia Tech. Accessed January 20, 2021. http://hdl.handle.net/10919/50647.

MLA Handbook (7th Edition):

Phillips, Tyrone. “Residual-based Discretization Error Estimation for Computational Fluid Dynamics.” 2014. Web. 20 Jan 2021.

Vancouver:

Phillips T. Residual-based Discretization Error Estimation for Computational Fluid Dynamics. [Internet] [Doctoral dissertation]. Virginia Tech; 2014. [cited 2021 Jan 20]. Available from: http://hdl.handle.net/10919/50647.

Council of Science Editors:

Phillips T. Residual-based Discretization Error Estimation for Computational Fluid Dynamics. [Doctoral Dissertation]. Virginia Tech; 2014. Available from: http://hdl.handle.net/10919/50647


Virginia Tech

10. Ohanian, Osgar John. Ducted Fan Aerodynamics and Modeling, with Applications of Steady and Synthetic Jet Flow Control.

Degree: PhD, Mechanical Engineering, 2011, Virginia Tech

 Ducted fan vehicles possess a superior ability to maximize payload capacity while minimizing vehicle size. Their ability to both hover and fly at high speed… (more)

Subjects/Keywords: non-dimensional; micro air vehicle; UAV; MAV; unmanned aerial vehicle; aerodynamic modeling; flow control; synthetic jets; rotor; shrouded propeller; ducted fan

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APA (6th Edition):

Ohanian, O. J. (2011). Ducted Fan Aerodynamics and Modeling, with Applications of Steady and Synthetic Jet Flow Control. (Doctoral Dissertation). Virginia Tech. Retrieved from http://hdl.handle.net/10919/27687

Chicago Manual of Style (16th Edition):

Ohanian, Osgar John. “Ducted Fan Aerodynamics and Modeling, with Applications of Steady and Synthetic Jet Flow Control.” 2011. Doctoral Dissertation, Virginia Tech. Accessed January 20, 2021. http://hdl.handle.net/10919/27687.

MLA Handbook (7th Edition):

Ohanian, Osgar John. “Ducted Fan Aerodynamics and Modeling, with Applications of Steady and Synthetic Jet Flow Control.” 2011. Web. 20 Jan 2021.

Vancouver:

Ohanian OJ. Ducted Fan Aerodynamics and Modeling, with Applications of Steady and Synthetic Jet Flow Control. [Internet] [Doctoral dissertation]. Virginia Tech; 2011. [cited 2021 Jan 20]. Available from: http://hdl.handle.net/10919/27687.

Council of Science Editors:

Ohanian OJ. Ducted Fan Aerodynamics and Modeling, with Applications of Steady and Synthetic Jet Flow Control. [Doctoral Dissertation]. Virginia Tech; 2011. Available from: http://hdl.handle.net/10919/27687


Virginia Tech

11. Meritt, Ryan James. A Study of Direct Measuring Skin Friction Gages for High Enthalpy Flow Applications.

Degree: MS, Aerospace and Ocean Engineering, 2010, Virginia Tech

 This study concerns the design, analysis, and initial testing of a novel skin friction gage for applications in three-dimensional, high-speed, high-enthalpy flows. Design conditions required… (more)

Subjects/Keywords: complex turbulent flow; aerodynamics; wall shear; skin friction; high-enthalpy

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APA (6th Edition):

Meritt, R. J. (2010). A Study of Direct Measuring Skin Friction Gages for High Enthalpy Flow Applications. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/76783

Chicago Manual of Style (16th Edition):

Meritt, Ryan James. “A Study of Direct Measuring Skin Friction Gages for High Enthalpy Flow Applications.” 2010. Masters Thesis, Virginia Tech. Accessed January 20, 2021. http://hdl.handle.net/10919/76783.

MLA Handbook (7th Edition):

Meritt, Ryan James. “A Study of Direct Measuring Skin Friction Gages for High Enthalpy Flow Applications.” 2010. Web. 20 Jan 2021.

Vancouver:

Meritt RJ. A Study of Direct Measuring Skin Friction Gages for High Enthalpy Flow Applications. [Internet] [Masters thesis]. Virginia Tech; 2010. [cited 2021 Jan 20]. Available from: http://hdl.handle.net/10919/76783.

Council of Science Editors:

Meritt RJ. A Study of Direct Measuring Skin Friction Gages for High Enthalpy Flow Applications. [Masters Thesis]. Virginia Tech; 2010. Available from: http://hdl.handle.net/10919/76783


Virginia Tech

12. Gundlach, John Frederick. Multidisciplinary Design Optimization and Industry Review of a 2010 Strut-Braced Wing Transonic Transport.

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

 Recent transonic airliner designs have generally converged upon a common cantilever low-wing configuration. It is unlikely that further large strides in performance are possible without… (more)

Subjects/Keywords: Multidisciplinary Design Optimization; Aircraft Design; Strut-Braced Wing; Transonic Transport

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APA (6th Edition):

Gundlach, J. F. (1999). Multidisciplinary Design Optimization and Industry Review of a 2010 Strut-Braced Wing Transonic Transport. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/33735

Chicago Manual of Style (16th Edition):

Gundlach, John Frederick. “Multidisciplinary Design Optimization and Industry Review of a 2010 Strut-Braced Wing Transonic Transport.” 1999. Masters Thesis, Virginia Tech. Accessed January 20, 2021. http://hdl.handle.net/10919/33735.

MLA Handbook (7th Edition):

Gundlach, John Frederick. “Multidisciplinary Design Optimization and Industry Review of a 2010 Strut-Braced Wing Transonic Transport.” 1999. Web. 20 Jan 2021.

Vancouver:

Gundlach JF. Multidisciplinary Design Optimization and Industry Review of a 2010 Strut-Braced Wing Transonic Transport. [Internet] [Masters thesis]. Virginia Tech; 1999. [cited 2021 Jan 20]. Available from: http://hdl.handle.net/10919/33735.

Council of Science Editors:

Gundlach JF. Multidisciplinary Design Optimization and Industry Review of a 2010 Strut-Braced Wing Transonic Transport. [Masters Thesis]. Virginia Tech; 1999. Available from: http://hdl.handle.net/10919/33735


Virginia Tech

13. Graf, Will Edward. Effects of Duct Lip Shaping and Various Control Devices on the Hover and Forward Flight Performance of Ducted Fan UAVs.

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

  The military's desire for ducted fan vertical takeoff and landing (VTOL) unmanned aerial vehicles (UAVs) stems from the vehicles' relatively small size, safety in… (more)

Subjects/Keywords: control effectors; ducted fan; UAV; duct lip shaping; stabilizer vanes; aerodynamics; control vanes

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APA (6th Edition):

Graf, W. E. (2005). Effects of Duct Lip Shaping and Various Control Devices on the Hover and Forward Flight Performance of Ducted Fan UAVs. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/33268

Chicago Manual of Style (16th Edition):

Graf, Will Edward. “Effects of Duct Lip Shaping and Various Control Devices on the Hover and Forward Flight Performance of Ducted Fan UAVs.” 2005. Masters Thesis, Virginia Tech. Accessed January 20, 2021. http://hdl.handle.net/10919/33268.

MLA Handbook (7th Edition):

Graf, Will Edward. “Effects of Duct Lip Shaping and Various Control Devices on the Hover and Forward Flight Performance of Ducted Fan UAVs.” 2005. Web. 20 Jan 2021.

Vancouver:

Graf WE. Effects of Duct Lip Shaping and Various Control Devices on the Hover and Forward Flight Performance of Ducted Fan UAVs. [Internet] [Masters thesis]. Virginia Tech; 2005. [cited 2021 Jan 20]. Available from: http://hdl.handle.net/10919/33268.

Council of Science Editors:

Graf WE. Effects of Duct Lip Shaping and Various Control Devices on the Hover and Forward Flight Performance of Ducted Fan UAVs. [Masters Thesis]. Virginia Tech; 2005. Available from: http://hdl.handle.net/10919/33268


Virginia Tech

14. MacMillin, Peter Edward. Trim, Control, and Performance Effects in Variable-Complexity High-Speed Civil Transport Design.

Degree: MS, Aerospace and Ocean Engineering, 1996, Virginia Tech

 Numerous trim, control requirements and mission generalizations have been made to our previous multidisciplinary design methodology for a high speed civil transport. We optimize the… (more)

Subjects/Keywords: none

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APA (6th Edition):

MacMillin, P. E. (1996). Trim, Control, and Performance Effects in Variable-Complexity High-Speed Civil Transport Design. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/36717

Chicago Manual of Style (16th Edition):

MacMillin, Peter Edward. “Trim, Control, and Performance Effects in Variable-Complexity High-Speed Civil Transport Design.” 1996. Masters Thesis, Virginia Tech. Accessed January 20, 2021. http://hdl.handle.net/10919/36717.

MLA Handbook (7th Edition):

MacMillin, Peter Edward. “Trim, Control, and Performance Effects in Variable-Complexity High-Speed Civil Transport Design.” 1996. Web. 20 Jan 2021.

Vancouver:

MacMillin PE. Trim, Control, and Performance Effects in Variable-Complexity High-Speed Civil Transport Design. [Internet] [Masters thesis]. Virginia Tech; 1996. [cited 2021 Jan 20]. Available from: http://hdl.handle.net/10919/36717.

Council of Science Editors:

MacMillin PE. Trim, Control, and Performance Effects in Variable-Complexity High-Speed Civil Transport Design. [Masters Thesis]. Virginia Tech; 1996. Available from: http://hdl.handle.net/10919/36717


Virginia Tech

15. Dippold, Vance Fredrick III. Numerical Assessment of the Performance of Jet-Wing Distributed Propulsion on Blended-Wing-Body Aircraft.

Degree: MS, Aerospace and Ocean Engineering, 2003, Virginia Tech

  Conventional airliners use two to four engines in a Cayley-type arrangement to provide thrust, and the thrust from these engines is typically concentrated right… (more)

Subjects/Keywords: Jet-Flap; Blended-Wing-Body; Computational Fluid Dynamics; Jet-Wing; Distributed Propulsion

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APA (6th Edition):

Dippold, V. F. I. (2003). Numerical Assessment of the Performance of Jet-Wing Distributed Propulsion on Blended-Wing-Body Aircraft. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/34878

Chicago Manual of Style (16th Edition):

Dippold, Vance Fredrick III. “Numerical Assessment of the Performance of Jet-Wing Distributed Propulsion on Blended-Wing-Body Aircraft.” 2003. Masters Thesis, Virginia Tech. Accessed January 20, 2021. http://hdl.handle.net/10919/34878.

MLA Handbook (7th Edition):

Dippold, Vance Fredrick III. “Numerical Assessment of the Performance of Jet-Wing Distributed Propulsion on Blended-Wing-Body Aircraft.” 2003. Web. 20 Jan 2021.

Vancouver:

Dippold VFI. Numerical Assessment of the Performance of Jet-Wing Distributed Propulsion on Blended-Wing-Body Aircraft. [Internet] [Masters thesis]. Virginia Tech; 2003. [cited 2021 Jan 20]. Available from: http://hdl.handle.net/10919/34878.

Council of Science Editors:

Dippold VFI. Numerical Assessment of the Performance of Jet-Wing Distributed Propulsion on Blended-Wing-Body Aircraft. [Masters Thesis]. Virginia Tech; 2003. Available from: http://hdl.handle.net/10919/34878


Virginia Tech

16. Hasan, Shahab. An object-oriented, PHIGS-based Internal Layout Module for aircraft design.

Degree: MS, Mechanical Engineering, 1993, Virginia Tech

 During the conceptual design phase, aircraft designers require tools to be able to quickly and accurately produce concepts that meet given requirements. These tools often… (more)

Subjects/Keywords: Object-oriented programming (Computer science); LD5655.V855 1993.H379

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APA (6th Edition):

Hasan, S. (1993). An object-oriented, PHIGS-based Internal Layout Module for aircraft design. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/41345

Chicago Manual of Style (16th Edition):

Hasan, Shahab. “An object-oriented, PHIGS-based Internal Layout Module for aircraft design.” 1993. Masters Thesis, Virginia Tech. Accessed January 20, 2021. http://hdl.handle.net/10919/41345.

MLA Handbook (7th Edition):

Hasan, Shahab. “An object-oriented, PHIGS-based Internal Layout Module for aircraft design.” 1993. Web. 20 Jan 2021.

Vancouver:

Hasan S. An object-oriented, PHIGS-based Internal Layout Module for aircraft design. [Internet] [Masters thesis]. Virginia Tech; 1993. [cited 2021 Jan 20]. Available from: http://hdl.handle.net/10919/41345.

Council of Science Editors:

Hasan S. An object-oriented, PHIGS-based Internal Layout Module for aircraft design. [Masters Thesis]. Virginia Tech; 1993. Available from: http://hdl.handle.net/10919/41345


Virginia Tech

17. Dasgupta, Amlan. Addition of Features to an Existing MDO Model for Containerships.

Degree: MS, Aerospace and Ocean Engineering, 2001, Virginia Tech

 Traditionally, the â Design Spiralâ is used for the design of ships. The design spiral endorses the concept that the design process is sequential and… (more)

Subjects/Keywords: MDO; Optimization; Containerships

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APA (6th Edition):

Dasgupta, A. (2001). Addition of Features to an Existing MDO Model for Containerships. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/33351

Chicago Manual of Style (16th Edition):

Dasgupta, Amlan. “Addition of Features to an Existing MDO Model for Containerships.” 2001. Masters Thesis, Virginia Tech. Accessed January 20, 2021. http://hdl.handle.net/10919/33351.

MLA Handbook (7th Edition):

Dasgupta, Amlan. “Addition of Features to an Existing MDO Model for Containerships.” 2001. Web. 20 Jan 2021.

Vancouver:

Dasgupta A. Addition of Features to an Existing MDO Model for Containerships. [Internet] [Masters thesis]. Virginia Tech; 2001. [cited 2021 Jan 20]. Available from: http://hdl.handle.net/10919/33351.

Council of Science Editors:

Dasgupta A. Addition of Features to an Existing MDO Model for Containerships. [Masters Thesis]. Virginia Tech; 2001. Available from: http://hdl.handle.net/10919/33351


Virginia Tech

18. Shafer, Daniel Manfred. Active and Passive Flow Control over the Flight Deck of Small Naval Vessels.

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

 Helicopter operations in the vicinity of small naval surface vessels often require excessive pilot workload. Because of the unsteady flow field and large mean velocity… (more)

Subjects/Keywords: backward facing step; frigate ship airwake; flow control; helicopter/ship operations; airwake

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APA (6th Edition):

Shafer, D. M. (2005). Active and Passive Flow Control over the Flight Deck of Small Naval Vessels. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/32427

Chicago Manual of Style (16th Edition):

Shafer, Daniel Manfred. “Active and Passive Flow Control over the Flight Deck of Small Naval Vessels.” 2005. Masters Thesis, Virginia Tech. Accessed January 20, 2021. http://hdl.handle.net/10919/32427.

MLA Handbook (7th Edition):

Shafer, Daniel Manfred. “Active and Passive Flow Control over the Flight Deck of Small Naval Vessels.” 2005. Web. 20 Jan 2021.

Vancouver:

Shafer DM. Active and Passive Flow Control over the Flight Deck of Small Naval Vessels. [Internet] [Masters thesis]. Virginia Tech; 2005. [cited 2021 Jan 20]. Available from: http://hdl.handle.net/10919/32427.

Council of Science Editors:

Shafer DM. Active and Passive Flow Control over the Flight Deck of Small Naval Vessels. [Masters Thesis]. Virginia Tech; 2005. Available from: http://hdl.handle.net/10919/32427


Virginia Tech

19. Iglesias, Sergio. Optimum Spanloads Incorporating Wing Structural Considerations And Formation Flying.

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

 The classic minimum induced drag spanload is not necessarily the best choice for an aircraft. For a single aircraft configuration, variations from the elliptic, minimum… (more)

Subjects/Keywords: formation flight; structural constraint; spanload optimization

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APA (6th Edition):

Iglesias, S. (2000). Optimum Spanloads Incorporating Wing Structural Considerations And Formation Flying. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/35718

Chicago Manual of Style (16th Edition):

Iglesias, Sergio. “Optimum Spanloads Incorporating Wing Structural Considerations And Formation Flying.” 2000. Masters Thesis, Virginia Tech. Accessed January 20, 2021. http://hdl.handle.net/10919/35718.

MLA Handbook (7th Edition):

Iglesias, Sergio. “Optimum Spanloads Incorporating Wing Structural Considerations And Formation Flying.” 2000. Web. 20 Jan 2021.

Vancouver:

Iglesias S. Optimum Spanloads Incorporating Wing Structural Considerations And Formation Flying. [Internet] [Masters thesis]. Virginia Tech; 2000. [cited 2021 Jan 20]. Available from: http://hdl.handle.net/10919/35718.

Council of Science Editors:

Iglesias S. Optimum Spanloads Incorporating Wing Structural Considerations And Formation Flying. [Masters Thesis]. Virginia Tech; 2000. Available from: http://hdl.handle.net/10919/35718


Virginia Tech

20. Angster, Scott Reed. An object-oriented, knowledge-based, non-procedural approach to multi-disciplinary, parametric, conceptual design.

Degree: MS, Mechanical Engineering, 1993, Virginia Tech

  The use of computers in the area of design and manufacturing is commonplace in industry. Many companies are turning to custom designed in-house software… (more)

Subjects/Keywords: Expert systems (Computer science); LD5655.V855 1993.A537

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APA (6th Edition):

Angster, S. R. (1993). An object-oriented, knowledge-based, non-procedural approach to multi-disciplinary, parametric, conceptual design. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/46138

Chicago Manual of Style (16th Edition):

Angster, Scott Reed. “An object-oriented, knowledge-based, non-procedural approach to multi-disciplinary, parametric, conceptual design.” 1993. Masters Thesis, Virginia Tech. Accessed January 20, 2021. http://hdl.handle.net/10919/46138.

MLA Handbook (7th Edition):

Angster, Scott Reed. “An object-oriented, knowledge-based, non-procedural approach to multi-disciplinary, parametric, conceptual design.” 1993. Web. 20 Jan 2021.

Vancouver:

Angster SR. An object-oriented, knowledge-based, non-procedural approach to multi-disciplinary, parametric, conceptual design. [Internet] [Masters thesis]. Virginia Tech; 1993. [cited 2021 Jan 20]. Available from: http://hdl.handle.net/10919/46138.

Council of Science Editors:

Angster SR. An object-oriented, knowledge-based, non-procedural approach to multi-disciplinary, parametric, conceptual design. [Masters Thesis]. Virginia Tech; 1993. Available from: http://hdl.handle.net/10919/46138


Virginia Tech

21. Henry, Michael Maier. Two-Dimensional Shock Sensitivity Analysis for Transonic Airfoils with Leading-edge and Trailing-edge Device Deflections.

Degree: MS, Aerospace Engineering, 2001, Virginia Tech

 This investigation, in consideration of the sudden separation increase involved in wing drop, was to determine if the incorporated 2-D airfoil exhibits abnormal shock sensitivity.… (more)

Subjects/Keywords: 2-D flow separation; device deflection; transonic airfoil; shock movement

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APA (6th Edition):

Henry, M. M. (2001). Two-Dimensional Shock Sensitivity Analysis for Transonic Airfoils with Leading-edge and Trailing-edge Device Deflections. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/30924

Chicago Manual of Style (16th Edition):

Henry, Michael Maier. “Two-Dimensional Shock Sensitivity Analysis for Transonic Airfoils with Leading-edge and Trailing-edge Device Deflections.” 2001. Masters Thesis, Virginia Tech. Accessed January 20, 2021. http://hdl.handle.net/10919/30924.

MLA Handbook (7th Edition):

Henry, Michael Maier. “Two-Dimensional Shock Sensitivity Analysis for Transonic Airfoils with Leading-edge and Trailing-edge Device Deflections.” 2001. Web. 20 Jan 2021.

Vancouver:

Henry MM. Two-Dimensional Shock Sensitivity Analysis for Transonic Airfoils with Leading-edge and Trailing-edge Device Deflections. [Internet] [Masters thesis]. Virginia Tech; 2001. [cited 2021 Jan 20]. Available from: http://hdl.handle.net/10919/30924.

Council of Science Editors:

Henry MM. Two-Dimensional Shock Sensitivity Analysis for Transonic Airfoils with Leading-edge and Trailing-edge Device Deflections. [Masters Thesis]. Virginia Tech; 2001. Available from: http://hdl.handle.net/10919/30924


Virginia Tech

22. Kay, Jacob. Control authority assessment in aircraft conceptual design.

Degree: MS, Aerospace Engineering, 1992, Virginia Tech

 All aircraft must meet controllability requirements to be certified for commercial use or adopted by the mi1itary. Aircraft maneuverability is often 1imited by control authority.… (more)

Subjects/Keywords: Airplanes; LD5655.V855 1992.K39

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APA (6th Edition):

Kay, J. (1992). Control authority assessment in aircraft conceptual design. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/41767

Chicago Manual of Style (16th Edition):

Kay, Jacob. “Control authority assessment in aircraft conceptual design.” 1992. Masters Thesis, Virginia Tech. Accessed January 20, 2021. http://hdl.handle.net/10919/41767.

MLA Handbook (7th Edition):

Kay, Jacob. “Control authority assessment in aircraft conceptual design.” 1992. Web. 20 Jan 2021.

Vancouver:

Kay J. Control authority assessment in aircraft conceptual design. [Internet] [Masters thesis]. Virginia Tech; 1992. [cited 2021 Jan 20]. Available from: http://hdl.handle.net/10919/41767.

Council of Science Editors:

Kay J. Control authority assessment in aircraft conceptual design. [Masters Thesis]. Virginia Tech; 1992. Available from: http://hdl.handle.net/10919/41767


Virginia Tech

23. Heim, Eugene Henry DeWendt. Development of Methods for Improved Data Integrity and Efficient Testing of Wind Tunnel Models for Dynamic Test Conditions in Unsteady and Nonlinear Flight Regimes.

Degree: MS, Aerospace and Ocean Engineering, 2003, Virginia Tech

 Todayâ s high performance aircraft are operating in expanded flight envelopes, often maneuvering at high angular rates at high angles-of-attack, even above maximum lift. Current… (more)

Subjects/Keywords: Static; Forced Oscillation; Data Integrity; Efficient Testing; Wind Tunnel Testing; Uncertainty

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APA (6th Edition):

Heim, E. H. D. (2003). Development of Methods for Improved Data Integrity and Efficient Testing of Wind Tunnel Models for Dynamic Test Conditions in Unsteady and Nonlinear Flight Regimes. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/31050

Chicago Manual of Style (16th Edition):

Heim, Eugene Henry DeWendt. “Development of Methods for Improved Data Integrity and Efficient Testing of Wind Tunnel Models for Dynamic Test Conditions in Unsteady and Nonlinear Flight Regimes.” 2003. Masters Thesis, Virginia Tech. Accessed January 20, 2021. http://hdl.handle.net/10919/31050.

MLA Handbook (7th Edition):

Heim, Eugene Henry DeWendt. “Development of Methods for Improved Data Integrity and Efficient Testing of Wind Tunnel Models for Dynamic Test Conditions in Unsteady and Nonlinear Flight Regimes.” 2003. Web. 20 Jan 2021.

Vancouver:

Heim EHD. Development of Methods for Improved Data Integrity and Efficient Testing of Wind Tunnel Models for Dynamic Test Conditions in Unsteady and Nonlinear Flight Regimes. [Internet] [Masters thesis]. Virginia Tech; 2003. [cited 2021 Jan 20]. Available from: http://hdl.handle.net/10919/31050.

Council of Science Editors:

Heim EHD. Development of Methods for Improved Data Integrity and Efficient Testing of Wind Tunnel Models for Dynamic Test Conditions in Unsteady and Nonlinear Flight Regimes. [Masters Thesis]. Virginia Tech; 2003. Available from: http://hdl.handle.net/10919/31050


Virginia Tech

24. Good, Matthew G. Development of a Variable Camber Compliant Aircraft Tail using Structural Optimization.

Degree: MS, Mechanical Engineering, 2004, Virginia Tech

 The objectives of the research presented in this thesis are the development of a seven degree-of-freedom morphing airplane and the design and integration of a… (more)

Subjects/Keywords: Variable Camber; Method of Moving Asymptote; Structural Optimization; Morphing Airplanes; Compliant Mechanism

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APA (6th Edition):

Good, M. G. (2004). Development of a Variable Camber Compliant Aircraft Tail using Structural Optimization. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/33976

Chicago Manual of Style (16th Edition):

Good, Matthew G. “Development of a Variable Camber Compliant Aircraft Tail using Structural Optimization.” 2004. Masters Thesis, Virginia Tech. Accessed January 20, 2021. http://hdl.handle.net/10919/33976.

MLA Handbook (7th Edition):

Good, Matthew G. “Development of a Variable Camber Compliant Aircraft Tail using Structural Optimization.” 2004. Web. 20 Jan 2021.

Vancouver:

Good MG. Development of a Variable Camber Compliant Aircraft Tail using Structural Optimization. [Internet] [Masters thesis]. Virginia Tech; 2004. [cited 2021 Jan 20]. Available from: http://hdl.handle.net/10919/33976.

Council of Science Editors:

Good MG. Development of a Variable Camber Compliant Aircraft Tail using Structural Optimization. [Masters Thesis]. Virginia Tech; 2004. Available from: http://hdl.handle.net/10919/33976


Virginia Tech

25. Ashley, Patrick A. Control power requirements for the velocity vector roll.

Degree: MS, Aerospace Engineering, 1994, Virginia Tech

  A method for determining the maximum control moments required for an aircraft to perform a velocity vector roll is investigated. The velocity vector roll… (more)

Subjects/Keywords: Rolling (Aerodynamics); LD5655.V855 1994.A845

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APA (6th Edition):

Ashley, P. A. (1994). Control power requirements for the velocity vector roll. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/46252

Chicago Manual of Style (16th Edition):

Ashley, Patrick A. “Control power requirements for the velocity vector roll.” 1994. Masters Thesis, Virginia Tech. Accessed January 20, 2021. http://hdl.handle.net/10919/46252.

MLA Handbook (7th Edition):

Ashley, Patrick A. “Control power requirements for the velocity vector roll.” 1994. Web. 20 Jan 2021.

Vancouver:

Ashley PA. Control power requirements for the velocity vector roll. [Internet] [Masters thesis]. Virginia Tech; 1994. [cited 2021 Jan 20]. Available from: http://hdl.handle.net/10919/46252.

Council of Science Editors:

Ashley PA. Control power requirements for the velocity vector roll. [Masters Thesis]. Virginia Tech; 1994. Available from: http://hdl.handle.net/10919/46252


Virginia Tech

26. Engel, Mark A. A wind tunnel investigation of a wing-tip trailing vortex.

Degree: MS, Aerospace Engineering, 1995, Virginia Tech

  A 3 'x2' subsonic wind tunnel has been constructed and calibrated. The flow in the wind tunnel accelerates 6.1 % along the test section… (more)

Subjects/Keywords: wind affect; LD5655.V855 1995.E544

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APA (6th Edition):

Engel, M. A. (1995). A wind tunnel investigation of a wing-tip trailing vortex. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/40571

Chicago Manual of Style (16th Edition):

Engel, Mark A. “A wind tunnel investigation of a wing-tip trailing vortex.” 1995. Masters Thesis, Virginia Tech. Accessed January 20, 2021. http://hdl.handle.net/10919/40571.

MLA Handbook (7th Edition):

Engel, Mark A. “A wind tunnel investigation of a wing-tip trailing vortex.” 1995. Web. 20 Jan 2021.

Vancouver:

Engel MA. A wind tunnel investigation of a wing-tip trailing vortex. [Internet] [Masters thesis]. Virginia Tech; 1995. [cited 2021 Jan 20]. Available from: http://hdl.handle.net/10919/40571.

Council of Science Editors:

Engel MA. A wind tunnel investigation of a wing-tip trailing vortex. [Masters Thesis]. Virginia Tech; 1995. Available from: http://hdl.handle.net/10919/40571


Virginia Tech

27. Keen, Ernest Brock. A Conceptual Design Methodology for Predicting the Aerodynamics of Upper Surface Blowing on Airfoils and Wings.

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

 One of the most promising powered-lift concepts is Upper Surface Blowing (USB), where the engines are placed above the wing and the engine exhaust jet… (more)

Subjects/Keywords: aerodynamics; conceptual design; USB; upper surface blowing

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APA (6th Edition):

Keen, E. B. (2004). A Conceptual Design Methodology for Predicting the Aerodynamics of Upper Surface Blowing on Airfoils and Wings. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/35999

Chicago Manual of Style (16th Edition):

Keen, Ernest Brock. “A Conceptual Design Methodology for Predicting the Aerodynamics of Upper Surface Blowing on Airfoils and Wings.” 2004. Masters Thesis, Virginia Tech. Accessed January 20, 2021. http://hdl.handle.net/10919/35999.

MLA Handbook (7th Edition):

Keen, Ernest Brock. “A Conceptual Design Methodology for Predicting the Aerodynamics of Upper Surface Blowing on Airfoils and Wings.” 2004. Web. 20 Jan 2021.

Vancouver:

Keen EB. A Conceptual Design Methodology for Predicting the Aerodynamics of Upper Surface Blowing on Airfoils and Wings. [Internet] [Masters thesis]. Virginia Tech; 2004. [cited 2021 Jan 20]. Available from: http://hdl.handle.net/10919/35999.

Council of Science Editors:

Keen EB. A Conceptual Design Methodology for Predicting the Aerodynamics of Upper Surface Blowing on Airfoils and Wings. [Masters Thesis]. Virginia Tech; 2004. Available from: http://hdl.handle.net/10919/35999


Virginia Tech

28. Liu, Ding-Jen. Experimental aerodynamic comparison of two magnetically levitated (MagLev) vehicle designs.

Degree: MS, Aerospace Engineering, 1995, Virginia Tech

  An experimental investigation was conducted to better understand the aerodynamics of magnetically levitated (MagLev) high speed vehicles operating in ground effect. A high speed… (more)

Subjects/Keywords: high speed vehicles; LD5655.V855 1995.L58

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APA (6th Edition):

Liu, D. (1995). Experimental aerodynamic comparison of two magnetically levitated (MagLev) vehicle designs. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/42913

Chicago Manual of Style (16th Edition):

Liu, Ding-Jen. “Experimental aerodynamic comparison of two magnetically levitated (MagLev) vehicle designs.” 1995. Masters Thesis, Virginia Tech. Accessed January 20, 2021. http://hdl.handle.net/10919/42913.

MLA Handbook (7th Edition):

Liu, Ding-Jen. “Experimental aerodynamic comparison of two magnetically levitated (MagLev) vehicle designs.” 1995. Web. 20 Jan 2021.

Vancouver:

Liu D. Experimental aerodynamic comparison of two magnetically levitated (MagLev) vehicle designs. [Internet] [Masters thesis]. Virginia Tech; 1995. [cited 2021 Jan 20]. Available from: http://hdl.handle.net/10919/42913.

Council of Science Editors:

Liu D. Experimental aerodynamic comparison of two magnetically levitated (MagLev) vehicle designs. [Masters Thesis]. Virginia Tech; 1995. Available from: http://hdl.handle.net/10919/42913


Virginia Tech

29. Saha, Nilanjan. Gap Size Effect on Low Reynolds Number Wind Tunnel Experiments.

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

 A system was designed to measure the effect of gap size on semi-span low Reynolds number wind tunnel experiments. The lift forces on NACA 1412,… (more)

Subjects/Keywords: wind tunnel; pressure distribution; Gap size

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APA (6th Edition):

Saha, N. (1999). Gap Size Effect on Low Reynolds Number Wind Tunnel Experiments. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/35938

Chicago Manual of Style (16th Edition):

Saha, Nilanjan. “Gap Size Effect on Low Reynolds Number Wind Tunnel Experiments.” 1999. Masters Thesis, Virginia Tech. Accessed January 20, 2021. http://hdl.handle.net/10919/35938.

MLA Handbook (7th Edition):

Saha, Nilanjan. “Gap Size Effect on Low Reynolds Number Wind Tunnel Experiments.” 1999. Web. 20 Jan 2021.

Vancouver:

Saha N. Gap Size Effect on Low Reynolds Number Wind Tunnel Experiments. [Internet] [Masters thesis]. Virginia Tech; 1999. [cited 2021 Jan 20]. Available from: http://hdl.handle.net/10919/35938.

Council of Science Editors:

Saha N. Gap Size Effect on Low Reynolds Number Wind Tunnel Experiments. [Masters Thesis]. Virginia Tech; 1999. Available from: http://hdl.handle.net/10919/35938


Virginia Tech

30. Crisafulli, Paul J. Response surface approximations for pitching moment including pitch-up in the multidisciplinary design optimization of a high-speed civil transport.

Degree: MS, Aerospace Engineering, 1996, Virginia Tech

see document Advisors/Committee Members: Mason, William H. (committeechair), Grossman, Bernard M. (committee member), Lutze, Frederick H. Jr. (committee member).

Subjects/Keywords: response surface methodology; LD5655.V855 1996.C757

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APA (6th Edition):

Crisafulli, P. J. (1996). Response surface approximations for pitching moment including pitch-up in the multidisciplinary design optimization of a high-speed civil transport. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/45070

Chicago Manual of Style (16th Edition):

Crisafulli, Paul J. “Response surface approximations for pitching moment including pitch-up in the multidisciplinary design optimization of a high-speed civil transport.” 1996. Masters Thesis, Virginia Tech. Accessed January 20, 2021. http://hdl.handle.net/10919/45070.

MLA Handbook (7th Edition):

Crisafulli, Paul J. “Response surface approximations for pitching moment including pitch-up in the multidisciplinary design optimization of a high-speed civil transport.” 1996. Web. 20 Jan 2021.

Vancouver:

Crisafulli PJ. Response surface approximations for pitching moment including pitch-up in the multidisciplinary design optimization of a high-speed civil transport. [Internet] [Masters thesis]. Virginia Tech; 1996. [cited 2021 Jan 20]. Available from: http://hdl.handle.net/10919/45070.

Council of Science Editors:

Crisafulli PJ. Response surface approximations for pitching moment including pitch-up in the multidisciplinary design optimization of a high-speed civil transport. [Masters Thesis]. Virginia Tech; 1996. Available from: http://hdl.handle.net/10919/45070

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