Advanced search options

Advanced Search Options 🞨

Browse by author name (“Author name starts with…”).

Find ETDs with:

in
/  
in
/  
in
/  
in

Written in Published in Earliest date Latest date

Sorted by

Results per page:

Sorted by: relevance · author · university · dateNew search

You searched for +publisher:"Virginia Tech" +contributor:("Mason, William H."). Showing records 1 – 30 of 111 total matches.

[1] [2] [3] [4]

Search Limiters

Last 2 Years | English Only

Degrees

Levels

▼ Search Limiters


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 and Ocean 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

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

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 October 23, 2019. 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. 23 Oct 2019.

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 2019 Oct 23]. 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. 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

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

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 October 23, 2019. 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. 23 Oct 2019.

Vancouver:

Meritt RJ. A Study of Direct Measuring Skin Friction Gages for High Enthalpy Flow Applications. [Internet] [Masters thesis]. Virginia Tech; 2010. [cited 2019 Oct 23]. 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

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

Degree: MS, Aerospace and Ocean 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

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

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 October 23, 2019. 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. 23 Oct 2019.

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 2019 Oct 23]. 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

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

Degree: MS, Aerospace and Ocean 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

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

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 October 23, 2019. 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. 23 Oct 2019.

Vancouver:

Knight KCD. Assessment of RANS Turbulence Models for Strut-Wing Junctions. [Internet] [Masters thesis]. Virginia Tech; 2011. [cited 2019 Oct 23]. 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

5. 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

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

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 October 23, 2019. 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. 23 Oct 2019.

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 2019 Oct 23]. 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

6. 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

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

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 October 23, 2019. 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. 23 Oct 2019.

Vancouver:

Walker WP. Optimization of Harmonically Deforming Thin Airfoils and Membrane Wings for Optimum Thrust and Efficiency. [Internet] [Doctoral dissertation]. Virginia Tech; 2012. [cited 2019 Oct 23]. 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

7. Veluri, Subrahmanya Pavan Kumar. Code Verification and Numerical Accuracy Assessment for Finite Volume CFD Codes.

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

 A detailed code verification study of an unstructured finite volume Computational Fluid Dynamics (CFD) code is performed. The Method of Manufactured Solutions is used to… (more)

Subjects/Keywords: Order of Accuracy; Computational Fluid Dynamics; Discretization Error; Method of Manufactured Solutions; Code Verification

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Veluri, S. P. K. (2010). Code Verification and Numerical Accuracy Assessment for Finite Volume CFD Codes. (Doctoral Dissertation). Virginia Tech. Retrieved from http://hdl.handle.net/10919/28715

Chicago Manual of Style (16th Edition):

Veluri, Subrahmanya Pavan Kumar. “Code Verification and Numerical Accuracy Assessment for Finite Volume CFD Codes.” 2010. Doctoral Dissertation, Virginia Tech. Accessed October 23, 2019. http://hdl.handle.net/10919/28715.

MLA Handbook (7th Edition):

Veluri, Subrahmanya Pavan Kumar. “Code Verification and Numerical Accuracy Assessment for Finite Volume CFD Codes.” 2010. Web. 23 Oct 2019.

Vancouver:

Veluri SPK. Code Verification and Numerical Accuracy Assessment for Finite Volume CFD Codes. [Internet] [Doctoral dissertation]. Virginia Tech; 2010. [cited 2019 Oct 23]. Available from: http://hdl.handle.net/10919/28715.

Council of Science Editors:

Veluri SPK. Code Verification and Numerical Accuracy Assessment for Finite Volume CFD Codes. [Doctoral Dissertation]. Virginia Tech; 2010. Available from: http://hdl.handle.net/10919/28715


Virginia Tech

8. 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

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

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 October 23, 2019. 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. 23 Oct 2019.

Vancouver:

Phillips T. Extrapolation-based Discretization Error and Uncertainty Estimation in Computational Fluid Dynamics. [Internet] [Masters thesis]. Virginia Tech; 2012. [cited 2019 Oct 23]. 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

9. 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

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

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 October 23, 2019. 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. 23 Oct 2019.

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 2019 Oct 23]. 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


Virginia Tech

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

Degree: PhD, Aerospace and Ocean 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

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

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 October 23, 2019. 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. 23 Oct 2019.

Vancouver:

Ghoman SS. A Hybrid Optimization Framework with POD-based Order Reduction and Design-Space Evolution Scheme. [Internet] [Doctoral dissertation]. Virginia Tech; 2013. [cited 2019 Oct 23]. 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

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

Degree: PhD, Aerospace and Ocean 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

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

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 October 23, 2019. http://hdl.handle.net/10919/50647.

MLA Handbook (7th Edition):

Phillips, Tyrone. “Residual-based Discretization Error Estimation for Computational Fluid Dynamics.” 2014. Web. 23 Oct 2019.

Vancouver:

Phillips T. Residual-based Discretization Error Estimation for Computational Fluid Dynamics. [Internet] [Doctoral dissertation]. Virginia Tech; 2014. [cited 2019 Oct 23]. 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

12. 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

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

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 October 23, 2019. 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. 23 Oct 2019.

Vancouver:

Ohanian OJ. Ducted Fan Aerodynamics and Modeling, with Applications of Steady and Synthetic Jet Flow Control. [Internet] [Doctoral dissertation]. Virginia Tech; 2011. [cited 2019 Oct 23]. 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

13. Cotting, Malcolm Christopher. Evolution of Flying Qualities Analysis: Problems for a New Generation of Aircraft.

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

  A number of challenges in the development and application of flying qualities criteria for modern aircraft are addressed in this dissertation. The history of… (more)

Subjects/Keywords: Education; Flight Mechanics; Flying Qualities; UAV

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Cotting, M. C. (2010). Evolution of Flying Qualities Analysis: Problems for a New Generation of Aircraft. (Doctoral Dissertation). Virginia Tech. Retrieved from http://hdl.handle.net/10919/26781

Chicago Manual of Style (16th Edition):

Cotting, Malcolm Christopher. “Evolution of Flying Qualities Analysis: Problems for a New Generation of Aircraft.” 2010. Doctoral Dissertation, Virginia Tech. Accessed October 23, 2019. http://hdl.handle.net/10919/26781.

MLA Handbook (7th Edition):

Cotting, Malcolm Christopher. “Evolution of Flying Qualities Analysis: Problems for a New Generation of Aircraft.” 2010. Web. 23 Oct 2019.

Vancouver:

Cotting MC. Evolution of Flying Qualities Analysis: Problems for a New Generation of Aircraft. [Internet] [Doctoral dissertation]. Virginia Tech; 2010. [cited 2019 Oct 23]. Available from: http://hdl.handle.net/10919/26781.

Council of Science Editors:

Cotting MC. Evolution of Flying Qualities Analysis: Problems for a New Generation of Aircraft. [Doctoral Dissertation]. Virginia Tech; 2010. Available from: http://hdl.handle.net/10919/26781


Virginia Tech

14. Varano, Nathaniel David. Fluid Dynamics and Surface Pressure Fluctuations of Turbulent Boundary Layers Over Sparse Roughness.

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

 Turbulent boundary layers over rough surfaces are a common, yet often overlooked, problem of practical engineering importance. Development of correlations between boundary layer parameters that… (more)

Subjects/Keywords: roughness; laser Doppler velocimetry; skin friction; turbulence; boundary layer; surface pressure

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Varano, N. D. (2010). Fluid Dynamics and Surface Pressure Fluctuations of Turbulent Boundary Layers Over Sparse Roughness. (Doctoral Dissertation). Virginia Tech. Retrieved from http://hdl.handle.net/10919/26918

Chicago Manual of Style (16th Edition):

Varano, Nathaniel David. “Fluid Dynamics and Surface Pressure Fluctuations of Turbulent Boundary Layers Over Sparse Roughness.” 2010. Doctoral Dissertation, Virginia Tech. Accessed October 23, 2019. http://hdl.handle.net/10919/26918.

MLA Handbook (7th Edition):

Varano, Nathaniel David. “Fluid Dynamics and Surface Pressure Fluctuations of Turbulent Boundary Layers Over Sparse Roughness.” 2010. Web. 23 Oct 2019.

Vancouver:

Varano ND. Fluid Dynamics and Surface Pressure Fluctuations of Turbulent Boundary Layers Over Sparse Roughness. [Internet] [Doctoral dissertation]. Virginia Tech; 2010. [cited 2019 Oct 23]. Available from: http://hdl.handle.net/10919/26918.

Council of Science Editors:

Varano ND. Fluid Dynamics and Surface Pressure Fluctuations of Turbulent Boundary Layers Over Sparse Roughness. [Doctoral Dissertation]. Virginia Tech; 2010. Available from: http://hdl.handle.net/10919/26918


Virginia Tech

15. Hopkins, Andrew. Fluid Dynamics and Surface Pressure Fluctuations of Two-Dimensional Turbulent Boundary Layers Over Densely Distributed Surface Roughness.

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

 Measurements were made in two-dimensional zero pressure gradient turbulent boundary layers over 5 geometries of three-dimensional densely distributed surface roughness. A 3-velocity component laser Doppler… (more)

Subjects/Keywords: von Karman Constant; Skin Friction; Boundary Layer; Turbulence; Surface Pressure Fluctuations; Laser Doppler Velocimetry; Surface Roughness

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Hopkins, A. (2010). Fluid Dynamics and Surface Pressure Fluctuations of Two-Dimensional Turbulent Boundary Layers Over Densely Distributed Surface Roughness. (Doctoral Dissertation). Virginia Tech. Retrieved from http://hdl.handle.net/10919/26919

Chicago Manual of Style (16th Edition):

Hopkins, Andrew. “Fluid Dynamics and Surface Pressure Fluctuations of Two-Dimensional Turbulent Boundary Layers Over Densely Distributed Surface Roughness.” 2010. Doctoral Dissertation, Virginia Tech. Accessed October 23, 2019. http://hdl.handle.net/10919/26919.

MLA Handbook (7th Edition):

Hopkins, Andrew. “Fluid Dynamics and Surface Pressure Fluctuations of Two-Dimensional Turbulent Boundary Layers Over Densely Distributed Surface Roughness.” 2010. Web. 23 Oct 2019.

Vancouver:

Hopkins A. Fluid Dynamics and Surface Pressure Fluctuations of Two-Dimensional Turbulent Boundary Layers Over Densely Distributed Surface Roughness. [Internet] [Doctoral dissertation]. Virginia Tech; 2010. [cited 2019 Oct 23]. Available from: http://hdl.handle.net/10919/26919.

Council of Science Editors:

Hopkins A. Fluid Dynamics and Surface Pressure Fluctuations of Two-Dimensional Turbulent Boundary Layers Over Densely Distributed Surface Roughness. [Doctoral Dissertation]. Virginia Tech; 2010. Available from: http://hdl.handle.net/10919/26919


Virginia Tech

16. Ko, Yan-Yee Andy. The Role of Constraints and Vehicle Concepts in Transport Design: A Comparison of Cantilever and Strut-Braced Wing Airplane Concepts.

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

 The purpose of this study is to examine the multidisciplinary design optimization (MDO) of a strut-braced wing (SBW) aircraft compared to similarly designed cantilever wing… (more)

Subjects/Keywords: Tip-Mounted Engines; Strut-Braced Wing; Aircraft Design; Multidisciplinary Design Optimization

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Ko, Y. A. (2000). The Role of Constraints and Vehicle Concepts in Transport Design: A Comparison of Cantilever and Strut-Braced Wing Airplane Concepts. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/32785

Chicago Manual of Style (16th Edition):

Ko, Yan-Yee Andy. “The Role of Constraints and Vehicle Concepts in Transport Design: A Comparison of Cantilever and Strut-Braced Wing Airplane Concepts.” 2000. Masters Thesis, Virginia Tech. Accessed October 23, 2019. http://hdl.handle.net/10919/32785.

MLA Handbook (7th Edition):

Ko, Yan-Yee Andy. “The Role of Constraints and Vehicle Concepts in Transport Design: A Comparison of Cantilever and Strut-Braced Wing Airplane Concepts.” 2000. Web. 23 Oct 2019.

Vancouver:

Ko YA. The Role of Constraints and Vehicle Concepts in Transport Design: A Comparison of Cantilever and Strut-Braced Wing Airplane Concepts. [Internet] [Masters thesis]. Virginia Tech; 2000. [cited 2019 Oct 23]. Available from: http://hdl.handle.net/10919/32785.

Council of Science Editors:

Ko YA. The Role of Constraints and Vehicle Concepts in Transport Design: A Comparison of Cantilever and Strut-Braced Wing Airplane Concepts. [Masters Thesis]. Virginia Tech; 2000. Available from: http://hdl.handle.net/10919/32785


Virginia Tech

17. 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

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

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 October 23, 2019. 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. 23 Oct 2019.

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 2019 Oct 23]. 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

18. 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

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

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 October 23, 2019. http://hdl.handle.net/10919/33351.

MLA Handbook (7th Edition):

Dasgupta, Amlan. “Addition of Features to an Existing MDO Model for Containerships.” 2001. Web. 23 Oct 2019.

Vancouver:

Dasgupta A. Addition of Features to an Existing MDO Model for Containerships. [Internet] [Masters thesis]. Virginia Tech; 2001. [cited 2019 Oct 23]. 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

19. Goel, Amit. Visualization in Problem Solving Environments.

Degree: MS, Computer Science, 1999, Virginia Tech

  This thesis describes two problem solving environments that integrate visualization and computational tools into a high level user interface. The objective of a problem… (more)

Subjects/Keywords: Problem solving environment; data visualization

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Goel, A. (1999). Visualization in Problem Solving Environments. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/33646

Chicago Manual of Style (16th Edition):

Goel, Amit. “Visualization in Problem Solving Environments.” 1999. Masters Thesis, Virginia Tech. Accessed October 23, 2019. http://hdl.handle.net/10919/33646.

MLA Handbook (7th Edition):

Goel, Amit. “Visualization in Problem Solving Environments.” 1999. Web. 23 Oct 2019.

Vancouver:

Goel A. Visualization in Problem Solving Environments. [Internet] [Masters thesis]. Virginia Tech; 1999. [cited 2019 Oct 23]. Available from: http://hdl.handle.net/10919/33646.

Council of Science Editors:

Goel A. Visualization in Problem Solving Environments. [Masters Thesis]. Virginia Tech; 1999. Available from: http://hdl.handle.net/10919/33646


Virginia Tech

20. Hinshaw, Tyler. Analysis and Design of a Morphing Wing Tip using Multicellular Flexible Matrix Composite Adaptive Skins.

Degree: MS, Aerospace and Ocean Engineering, 2009, Virginia Tech

 The material presented in this thesis uses concepts of the finite element and doublet panel methods to develop a structural-aerodynamic coupled mathematical model for the… (more)

Subjects/Keywords: Morphing Wing; Skins; Intelligent Structures

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Hinshaw, T. (2009). Analysis and Design of a Morphing Wing Tip using Multicellular Flexible Matrix Composite Adaptive Skins. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/33932

Chicago Manual of Style (16th Edition):

Hinshaw, Tyler. “Analysis and Design of a Morphing Wing Tip using Multicellular Flexible Matrix Composite Adaptive Skins.” 2009. Masters Thesis, Virginia Tech. Accessed October 23, 2019. http://hdl.handle.net/10919/33932.

MLA Handbook (7th Edition):

Hinshaw, Tyler. “Analysis and Design of a Morphing Wing Tip using Multicellular Flexible Matrix Composite Adaptive Skins.” 2009. Web. 23 Oct 2019.

Vancouver:

Hinshaw T. Analysis and Design of a Morphing Wing Tip using Multicellular Flexible Matrix Composite Adaptive Skins. [Internet] [Masters thesis]. Virginia Tech; 2009. [cited 2019 Oct 23]. Available from: http://hdl.handle.net/10919/33932.

Council of Science Editors:

Hinshaw T. Analysis and Design of a Morphing Wing Tip using Multicellular Flexible Matrix Composite Adaptive Skins. [Masters Thesis]. Virginia Tech; 2009. Available from: http://hdl.handle.net/10919/33932


Virginia Tech

21. 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

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

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 October 23, 2019. 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. 23 Oct 2019.

Vancouver:

Good MG. Development of a Variable Camber Compliant Aircraft Tail using Structural Optimization. [Internet] [Masters thesis]. Virginia Tech; 2004. [cited 2019 Oct 23]. 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

22. Ganesan, Vikram. A Model for Multidisciplinary Optimization for Containerships.

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

 This thesis describes a multidisciplinary design optimization approach to containership design. The method employs widely accepted regression equations for computing resistance, weights, building costs and… (more)

Subjects/Keywords: Optimization; Containerships; Multidisciplinary

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Ganesan, V. (1999). A Model for Multidisciplinary Optimization for Containerships. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/34151

Chicago Manual of Style (16th Edition):

Ganesan, Vikram. “A Model for Multidisciplinary Optimization for Containerships.” 1999. Masters Thesis, Virginia Tech. Accessed October 23, 2019. http://hdl.handle.net/10919/34151.

MLA Handbook (7th Edition):

Ganesan, Vikram. “A Model for Multidisciplinary Optimization for Containerships.” 1999. Web. 23 Oct 2019.

Vancouver:

Ganesan V. A Model for Multidisciplinary Optimization for Containerships. [Internet] [Masters thesis]. Virginia Tech; 1999. [cited 2019 Oct 23]. Available from: http://hdl.handle.net/10919/34151.

Council of Science Editors:

Ganesan V. A Model for Multidisciplinary Optimization for Containerships. [Masters Thesis]. Virginia Tech; 1999. Available from: http://hdl.handle.net/10919/34151


Virginia Tech

23. Harrison, Neal A. Active Flow Control of a Boundary Layer Ingesting Serpentine Diffuser.

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

 The use of serpentine boundary layer ingesting (BLI) diffusers offers a significant benefit to the performance of Blended Wing Body aircraft. However, the inherent diffuser… (more)

Subjects/Keywords: boundary layer ingestion; swirl; BLI; AFC; flow control; serpentine; aerodynamics; active; diffuser; inlet; duct; distortion

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Harrison, N. A. (2005). Active Flow Control of a Boundary Layer Ingesting Serpentine Diffuser. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/34163

Chicago Manual of Style (16th Edition):

Harrison, Neal A. “Active Flow Control of a Boundary Layer Ingesting Serpentine Diffuser.” 2005. Masters Thesis, Virginia Tech. Accessed October 23, 2019. http://hdl.handle.net/10919/34163.

MLA Handbook (7th Edition):

Harrison, Neal A. “Active Flow Control of a Boundary Layer Ingesting Serpentine Diffuser.” 2005. Web. 23 Oct 2019.

Vancouver:

Harrison NA. Active Flow Control of a Boundary Layer Ingesting Serpentine Diffuser. [Internet] [Masters thesis]. Virginia Tech; 2005. [cited 2019 Oct 23]. Available from: http://hdl.handle.net/10919/34163.

Council of Science Editors:

Harrison NA. Active Flow Control of a Boundary Layer Ingesting Serpentine Diffuser. [Masters Thesis]. Virginia Tech; 2005. Available from: http://hdl.handle.net/10919/34163


Virginia Tech

24. Morrow, Michael Thomas. A Self-Sustaining, Boundary-Layer-Adapted System for Terrain Exploration and Environmental Sampling.

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

 This thesis describes the preliminary design of a system for remote terrain exploration and environmental sampling on worlds with dense atmospheres. The motivation for the… (more)

Subjects/Keywords: boundary layer; internal actuation; inboard wing; Titan; terrain exploration; buoyancy-driven gliding

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Morrow, M. T. (2005). A Self-Sustaining, Boundary-Layer-Adapted System for Terrain Exploration and Environmental Sampling. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/34186

Chicago Manual of Style (16th Edition):

Morrow, Michael Thomas. “A Self-Sustaining, Boundary-Layer-Adapted System for Terrain Exploration and Environmental Sampling.” 2005. Masters Thesis, Virginia Tech. Accessed October 23, 2019. http://hdl.handle.net/10919/34186.

MLA Handbook (7th Edition):

Morrow, Michael Thomas. “A Self-Sustaining, Boundary-Layer-Adapted System for Terrain Exploration and Environmental Sampling.” 2005. Web. 23 Oct 2019.

Vancouver:

Morrow MT. A Self-Sustaining, Boundary-Layer-Adapted System for Terrain Exploration and Environmental Sampling. [Internet] [Masters thesis]. Virginia Tech; 2005. [cited 2019 Oct 23]. Available from: http://hdl.handle.net/10919/34186.

Council of Science Editors:

Morrow MT. A Self-Sustaining, Boundary-Layer-Adapted System for Terrain Exploration and Environmental Sampling. [Masters Thesis]. Virginia Tech; 2005. Available from: http://hdl.handle.net/10919/34186


Virginia Tech

25. Walker, Jessica Nicole. Numerical Studies of Jet-Wing Distributed Propulsion and a Simplified Noise Metric Method.

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

  In recent years, the aircraft industry has begun to focus its research capabilities on reducing emissions and noise produced by aircraft. Modern aircraft use… (more)

Subjects/Keywords: Computational Fluid Dynamics; Jet-Flap; Trailing Edge Noise; Jet-Wing; Distributed Propulsion

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Walker, J. N. (2004). Numerical Studies of Jet-Wing Distributed Propulsion and a Simplified Noise Metric Method. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/34752

Chicago Manual of Style (16th Edition):

Walker, Jessica Nicole. “Numerical Studies of Jet-Wing Distributed Propulsion and a Simplified Noise Metric Method.” 2004. Masters Thesis, Virginia Tech. Accessed October 23, 2019. http://hdl.handle.net/10919/34752.

MLA Handbook (7th Edition):

Walker, Jessica Nicole. “Numerical Studies of Jet-Wing Distributed Propulsion and a Simplified Noise Metric Method.” 2004. Web. 23 Oct 2019.

Vancouver:

Walker JN. Numerical Studies of Jet-Wing Distributed Propulsion and a Simplified Noise Metric Method. [Internet] [Masters thesis]. Virginia Tech; 2004. [cited 2019 Oct 23]. Available from: http://hdl.handle.net/10919/34752.

Council of Science Editors:

Walker JN. Numerical Studies of Jet-Wing Distributed Propulsion and a Simplified Noise Metric Method. [Masters Thesis]. Virginia Tech; 2004. Available from: http://hdl.handle.net/10919/34752


Virginia Tech

26. Dippold III, Vance Fredrick. 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

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Dippold III, V. F. (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 III, Vance Fredrick. “Numerical Assessment of the Performance of Jet-Wing Distributed Propulsion on Blended-Wing-Body Aircraft.” 2003. Masters Thesis, Virginia Tech. Accessed October 23, 2019. http://hdl.handle.net/10919/34878.

MLA Handbook (7th Edition):

Dippold III, Vance Fredrick. “Numerical Assessment of the Performance of Jet-Wing Distributed Propulsion on Blended-Wing-Body Aircraft.” 2003. Web. 23 Oct 2019.

Vancouver:

Dippold III VF. Numerical Assessment of the Performance of Jet-Wing Distributed Propulsion on Blended-Wing-Body Aircraft. [Internet] [Masters thesis]. Virginia Tech; 2003. [cited 2019 Oct 23]. Available from: http://hdl.handle.net/10919/34878.

Council of Science Editors:

Dippold III VF. 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

27. Waclawicz, Kevin. The Investigation of Crossflow Velocity and Off-the-Surface Streamtrace Topology for a Moderately Swept Wing at Transonic Mach Numbers.

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

 The purpose of this thesis is to investigate the crossflow and off-the-surface velocity traces on a moderately swept wing at transonic Mach numbers. Computational Fluid… (more)

Subjects/Keywords: Flow Topology; Separation; Off-the-Surface Flow

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Waclawicz, K. (2001). The Investigation of Crossflow Velocity and Off-the-Surface Streamtrace Topology for a Moderately Swept Wing at Transonic Mach Numbers. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/34941

Chicago Manual of Style (16th Edition):

Waclawicz, Kevin. “The Investigation of Crossflow Velocity and Off-the-Surface Streamtrace Topology for a Moderately Swept Wing at Transonic Mach Numbers.” 2001. Masters Thesis, Virginia Tech. Accessed October 23, 2019. http://hdl.handle.net/10919/34941.

MLA Handbook (7th Edition):

Waclawicz, Kevin. “The Investigation of Crossflow Velocity and Off-the-Surface Streamtrace Topology for a Moderately Swept Wing at Transonic Mach Numbers.” 2001. Web. 23 Oct 2019.

Vancouver:

Waclawicz K. The Investigation of Crossflow Velocity and Off-the-Surface Streamtrace Topology for a Moderately Swept Wing at Transonic Mach Numbers. [Internet] [Masters thesis]. Virginia Tech; 2001. [cited 2019 Oct 23]. Available from: http://hdl.handle.net/10919/34941.

Council of Science Editors:

Waclawicz K. The Investigation of Crossflow Velocity and Off-the-Surface Streamtrace Topology for a Moderately Swept Wing at Transonic Mach Numbers. [Masters Thesis]. Virginia Tech; 2001. Available from: http://hdl.handle.net/10919/34941


Virginia Tech

28. 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

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

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 October 23, 2019. http://hdl.handle.net/10919/35718.

MLA Handbook (7th Edition):

Iglesias, Sergio. “Optimum Spanloads Incorporating Wing Structural Considerations And Formation Flying.” 2000. Web. 23 Oct 2019.

Vancouver:

Iglesias S. Optimum Spanloads Incorporating Wing Structural Considerations And Formation Flying. [Internet] [Masters thesis]. Virginia Tech; 2000. [cited 2019 Oct 23]. 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

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

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

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 October 23, 2019. http://hdl.handle.net/10919/35938.

MLA Handbook (7th Edition):

Saha, Nilanjan. “Gap Size Effect on Low Reynolds Number Wind Tunnel Experiments.” 1999. Web. 23 Oct 2019.

Vancouver:

Saha N. Gap Size Effect on Low Reynolds Number Wind Tunnel Experiments. [Internet] [Masters thesis]. Virginia Tech; 1999. [cited 2019 Oct 23]. 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. 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

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

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 October 23, 2019. 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. 23 Oct 2019.

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 2019 Oct 23]. 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

[1] [2] [3] [4]

.