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You searched for +publisher:"North Carolina State University" +contributor:("Dr. Ashok Gopalarathnam, Committee Chair"). Showing records 1 – 11 of 11 total matches.

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North Carolina State University

1. Mukherjee, Rinku. Post-Stall Prediction of Multiple-Lifting-Surface Configurations Using a Decambering Approach.

Degree: PhD, Aerospace Engineering, 2004, North Carolina State University

 A novel scheme is presented for an iterative decambering approach to predict the post-stall characteristics of wings using known section data as inputs. The new… (more)

Subjects/Keywords: approach; decambering; configuration; Surface; Lifting; Multiple; Prediction; Post-Stall

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APA (6th Edition):

Mukherjee, R. (2004). Post-Stall Prediction of Multiple-Lifting-Surface Configurations Using a Decambering Approach. (Doctoral Dissertation). North Carolina State University. Retrieved from http://www.lib.ncsu.edu/resolver/1840.16/5100

Chicago Manual of Style (16th Edition):

Mukherjee, Rinku. “Post-Stall Prediction of Multiple-Lifting-Surface Configurations Using a Decambering Approach.” 2004. Doctoral Dissertation, North Carolina State University. Accessed November 14, 2019. http://www.lib.ncsu.edu/resolver/1840.16/5100.

MLA Handbook (7th Edition):

Mukherjee, Rinku. “Post-Stall Prediction of Multiple-Lifting-Surface Configurations Using a Decambering Approach.” 2004. Web. 14 Nov 2019.

Vancouver:

Mukherjee R. Post-Stall Prediction of Multiple-Lifting-Surface Configurations Using a Decambering Approach. [Internet] [Doctoral dissertation]. North Carolina State University; 2004. [cited 2019 Nov 14]. Available from: http://www.lib.ncsu.edu/resolver/1840.16/5100.

Council of Science Editors:

Mukherjee R. Post-Stall Prediction of Multiple-Lifting-Surface Configurations Using a Decambering Approach. [Doctoral Dissertation]. North Carolina State University; 2004. Available from: http://www.lib.ncsu.edu/resolver/1840.16/5100


North Carolina State University

2. Short, Seth Ryan. Modeling and Analysis of Active Turbulators on Low Reynolds Number Unmanned Aerial Vehicles.

Degree: MS, Aerospace Engineering, 2008, North Carolina State University

 ABSTRACT SETH RYAN SHORT. Modeling and Analysis of Active Turbulators on Low Reynolds Number Unmanned Aerial Vehicles. (Under the direction of Dr. Ashok Gopalarathnam.) The… (more)

Subjects/Keywords: turbulators; performance; UAV; trips; low Reynolds number

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APA (6th Edition):

Short, S. R. (2008). Modeling and Analysis of Active Turbulators on Low Reynolds Number Unmanned Aerial Vehicles. (Thesis). North Carolina State University. Retrieved from http://www.lib.ncsu.edu/resolver/1840.16/1711

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Chicago Manual of Style (16th Edition):

Short, Seth Ryan. “Modeling and Analysis of Active Turbulators on Low Reynolds Number Unmanned Aerial Vehicles.” 2008. Thesis, North Carolina State University. Accessed November 14, 2019. http://www.lib.ncsu.edu/resolver/1840.16/1711.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

MLA Handbook (7th Edition):

Short, Seth Ryan. “Modeling and Analysis of Active Turbulators on Low Reynolds Number Unmanned Aerial Vehicles.” 2008. Web. 14 Nov 2019.

Vancouver:

Short SR. Modeling and Analysis of Active Turbulators on Low Reynolds Number Unmanned Aerial Vehicles. [Internet] [Thesis]. North Carolina State University; 2008. [cited 2019 Nov 14]. Available from: http://www.lib.ncsu.edu/resolver/1840.16/1711.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Council of Science Editors:

Short SR. Modeling and Analysis of Active Turbulators on Low Reynolds Number Unmanned Aerial Vehicles. [Thesis]. North Carolina State University; 2008. Available from: http://www.lib.ncsu.edu/resolver/1840.16/1711

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation


North Carolina State University

3. Cusher, Aaron Anthony. Ideal Lift Distributions and Flap Settings for Adaptive Tailless Aircraft.

Degree: MS, Aerospace Engineering, 2006, North Carolina State University

 With ever increasing maturity in the field of subsonic aircraft design, there exists the desire to tailor the performance of an aircraft to suit specific… (more)

Subjects/Keywords: Adaptive; Flap Settings; Lift Distributions; Ideal; Tailless Aircraft

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APA (6th Edition):

Cusher, A. A. (2006). Ideal Lift Distributions and Flap Settings for Adaptive Tailless Aircraft. (Thesis). North Carolina State University. Retrieved from http://www.lib.ncsu.edu/resolver/1840.16/1803

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Chicago Manual of Style (16th Edition):

Cusher, Aaron Anthony. “Ideal Lift Distributions and Flap Settings for Adaptive Tailless Aircraft.” 2006. Thesis, North Carolina State University. Accessed November 14, 2019. http://www.lib.ncsu.edu/resolver/1840.16/1803.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

MLA Handbook (7th Edition):

Cusher, Aaron Anthony. “Ideal Lift Distributions and Flap Settings for Adaptive Tailless Aircraft.” 2006. Web. 14 Nov 2019.

Vancouver:

Cusher AA. Ideal Lift Distributions and Flap Settings for Adaptive Tailless Aircraft. [Internet] [Thesis]. North Carolina State University; 2006. [cited 2019 Nov 14]. Available from: http://www.lib.ncsu.edu/resolver/1840.16/1803.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Council of Science Editors:

Cusher AA. Ideal Lift Distributions and Flap Settings for Adaptive Tailless Aircraft. [Thesis]. North Carolina State University; 2006. Available from: http://www.lib.ncsu.edu/resolver/1840.16/1803

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation


North Carolina State University

4. McGowan, Gregory Zar. Computational Analysis of Circulation Control Airfoils.

Degree: MS, Aerospace Engineering, 2004, North Carolina State University

 Current projections for future aircraft concepts call for stringent requirements on high-lift and low cruise-drag. The purpose of this study is to examine the use… (more)

Subjects/Keywords: Circulation Control; airfoils; laminar flow

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APA (6th Edition):

McGowan, G. Z. (2004). Computational Analysis of Circulation Control Airfoils. (Thesis). North Carolina State University. Retrieved from http://www.lib.ncsu.edu/resolver/1840.16/2508

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Chicago Manual of Style (16th Edition):

McGowan, Gregory Zar. “Computational Analysis of Circulation Control Airfoils.” 2004. Thesis, North Carolina State University. Accessed November 14, 2019. http://www.lib.ncsu.edu/resolver/1840.16/2508.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

MLA Handbook (7th Edition):

McGowan, Gregory Zar. “Computational Analysis of Circulation Control Airfoils.” 2004. Web. 14 Nov 2019.

Vancouver:

McGowan GZ. Computational Analysis of Circulation Control Airfoils. [Internet] [Thesis]. North Carolina State University; 2004. [cited 2019 Nov 14]. Available from: http://www.lib.ncsu.edu/resolver/1840.16/2508.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Council of Science Editors:

McGowan GZ. Computational Analysis of Circulation Control Airfoils. [Thesis]. North Carolina State University; 2004. Available from: http://www.lib.ncsu.edu/resolver/1840.16/2508

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation


North Carolina State University

5. McAvoy, Christopher William. Analytical and Experimental Approaches to Airfoil-Aircraft Design Integration.

Degree: MS, Aerospace Engineering, 2002, North Carolina State University

 The aerodynamic characteristics of the wing airfoil are critical to achieving desired aircraft performance. However, even with all of the advances in airfoil and aircraft… (more)

Subjects/Keywords: aircraft performance; airfoil; aircraft; design; newton method; optimization; laminar flow; cruise flap; automatic flap; camber; trailing-edge flap; subsonic; general aviation; thin airfoil theory; UAV; stagnation point; low speed flow; low reynolds number; wind tunnel; NLF; drag polar; drag bucket; XFOIL; low-drag range; design integration; aerospace engineering; aeronautical; airfoil model construction; pressure distributions; trim effects; trim considerations; surface pressure sensing

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APA (6th Edition):

McAvoy, C. W. (2002). Analytical and Experimental Approaches to Airfoil-Aircraft Design Integration. (Thesis). North Carolina State University. Retrieved from http://www.lib.ncsu.edu/resolver/1840.16/7

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Chicago Manual of Style (16th Edition):

McAvoy, Christopher William. “Analytical and Experimental Approaches to Airfoil-Aircraft Design Integration.” 2002. Thesis, North Carolina State University. Accessed November 14, 2019. http://www.lib.ncsu.edu/resolver/1840.16/7.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

MLA Handbook (7th Edition):

McAvoy, Christopher William. “Analytical and Experimental Approaches to Airfoil-Aircraft Design Integration.” 2002. Web. 14 Nov 2019.

Vancouver:

McAvoy CW. Analytical and Experimental Approaches to Airfoil-Aircraft Design Integration. [Internet] [Thesis]. North Carolina State University; 2002. [cited 2019 Nov 14]. Available from: http://www.lib.ncsu.edu/resolver/1840.16/7.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Council of Science Editors:

McAvoy CW. Analytical and Experimental Approaches to Airfoil-Aircraft Design Integration. [Thesis]. North Carolina State University; 2002. Available from: http://www.lib.ncsu.edu/resolver/1840.16/7

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation


North Carolina State University

6. Segawa, Hidehiro. Optimum Flap Angles for Roll Control on Wings with Multiple Trailing-Edge Flaps.

Degree: MS, Aerospace Engineering, 2007, North Carolina State University

 This research effort explores the use of multiple trailing-edge flaps for efficiently generating rolling moment on aircraft. Using the concept of basic and additional lift… (more)

Subjects/Keywords: Trailing-Edge; Multiple; Wing; Control; Roll; Angles; Flap; Optimum

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APA (6th Edition):

Segawa, H. (2007). Optimum Flap Angles for Roll Control on Wings with Multiple Trailing-Edge Flaps. (Thesis). North Carolina State University. Retrieved from http://www.lib.ncsu.edu/resolver/1840.16/384

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Chicago Manual of Style (16th Edition):

Segawa, Hidehiro. “Optimum Flap Angles for Roll Control on Wings with Multiple Trailing-Edge Flaps.” 2007. Thesis, North Carolina State University. Accessed November 14, 2019. http://www.lib.ncsu.edu/resolver/1840.16/384.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

MLA Handbook (7th Edition):

Segawa, Hidehiro. “Optimum Flap Angles for Roll Control on Wings with Multiple Trailing-Edge Flaps.” 2007. Web. 14 Nov 2019.

Vancouver:

Segawa H. Optimum Flap Angles for Roll Control on Wings with Multiple Trailing-Edge Flaps. [Internet] [Thesis]. North Carolina State University; 2007. [cited 2019 Nov 14]. Available from: http://www.lib.ncsu.edu/resolver/1840.16/384.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Council of Science Editors:

Segawa H. Optimum Flap Angles for Roll Control on Wings with Multiple Trailing-Edge Flaps. [Thesis]. North Carolina State University; 2007. Available from: http://www.lib.ncsu.edu/resolver/1840.16/384

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation


North Carolina State University

7. Vosburg, Victor Jay. The Stability and Control of an Aircraft with an Adaptive Wing.

Degree: MS, Aerospace Engineering, 2005, North Carolina State University

 With increasing interest in the use of adaptive lifting surfaces for improved aircraft performance, it is necessary to study the stability and control characteristics of… (more)

Subjects/Keywords: AeroSim; Adaptive Wing; Stability and Control

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APA (6th Edition):

Vosburg, V. J. (2005). The Stability and Control of an Aircraft with an Adaptive Wing. (Thesis). North Carolina State University. Retrieved from http://www.lib.ncsu.edu/resolver/1840.16/1932

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Chicago Manual of Style (16th Edition):

Vosburg, Victor Jay. “The Stability and Control of an Aircraft with an Adaptive Wing.” 2005. Thesis, North Carolina State University. Accessed November 14, 2019. http://www.lib.ncsu.edu/resolver/1840.16/1932.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

MLA Handbook (7th Edition):

Vosburg, Victor Jay. “The Stability and Control of an Aircraft with an Adaptive Wing.” 2005. Web. 14 Nov 2019.

Vancouver:

Vosburg VJ. The Stability and Control of an Aircraft with an Adaptive Wing. [Internet] [Thesis]. North Carolina State University; 2005. [cited 2019 Nov 14]. Available from: http://www.lib.ncsu.edu/resolver/1840.16/1932.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Council of Science Editors:

Vosburg VJ. The Stability and Control of an Aircraft with an Adaptive Wing. [Thesis]. North Carolina State University; 2005. Available from: http://www.lib.ncsu.edu/resolver/1840.16/1932

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation


North Carolina State University

8. McGowan, Gregory Zar. Analytical and Computational Investigations of Airfoils Undergoing High-Frequency Sinusoidal Pitch and Plunge Motions at Low Reynolds Numbers.

Degree: PhD, Aerospace Engineering, 2008, North Carolina State University

 Current interests in Micro Air Vehicle (MAV)technologies call for the development of aerodynamic-design tools that will aid in the design of more efficient platforms that… (more)

Subjects/Keywords: unsteady aerodynamics; airfoil; CFD; flapping flight; low Reynolds number

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

APA (6th Edition):

McGowan, G. Z. (2008). Analytical and Computational Investigations of Airfoils Undergoing High-Frequency Sinusoidal Pitch and Plunge Motions at Low Reynolds Numbers. (Doctoral Dissertation). North Carolina State University. Retrieved from http://www.lib.ncsu.edu/resolver/1840.16/5678

Chicago Manual of Style (16th Edition):

McGowan, Gregory Zar. “Analytical and Computational Investigations of Airfoils Undergoing High-Frequency Sinusoidal Pitch and Plunge Motions at Low Reynolds Numbers.” 2008. Doctoral Dissertation, North Carolina State University. Accessed November 14, 2019. http://www.lib.ncsu.edu/resolver/1840.16/5678.

MLA Handbook (7th Edition):

McGowan, Gregory Zar. “Analytical and Computational Investigations of Airfoils Undergoing High-Frequency Sinusoidal Pitch and Plunge Motions at Low Reynolds Numbers.” 2008. Web. 14 Nov 2019.

Vancouver:

McGowan GZ. Analytical and Computational Investigations of Airfoils Undergoing High-Frequency Sinusoidal Pitch and Plunge Motions at Low Reynolds Numbers. [Internet] [Doctoral dissertation]. North Carolina State University; 2008. [cited 2019 Nov 14]. Available from: http://www.lib.ncsu.edu/resolver/1840.16/5678.

Council of Science Editors:

McGowan GZ. Analytical and Computational Investigations of Airfoils Undergoing High-Frequency Sinusoidal Pitch and Plunge Motions at Low Reynolds Numbers. [Doctoral Dissertation]. North Carolina State University; 2008. Available from: http://www.lib.ncsu.edu/resolver/1840.16/5678


North Carolina State University

9. King, Rachel Marie. On the Use of Wing Adaptation and Formation for Improved Aerodynamic Efficiency.

Degree: PhD, Aerospace Engineering, 2005, North Carolina State University

 There is a continuous effort to improve the performance and efficiency of today's aircraft, and the reduction of aircraft drag has been the primary focus… (more)

Subjects/Keywords: aerodynamic efficiency; adaptive wing; formation flight; ground-effect flight

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

APA (6th Edition):

King, R. M. (2005). On the Use of Wing Adaptation and Formation for Improved Aerodynamic Efficiency. (Doctoral Dissertation). North Carolina State University. Retrieved from http://www.lib.ncsu.edu/resolver/1840.16/5759

Chicago Manual of Style (16th Edition):

King, Rachel Marie. “On the Use of Wing Adaptation and Formation for Improved Aerodynamic Efficiency.” 2005. Doctoral Dissertation, North Carolina State University. Accessed November 14, 2019. http://www.lib.ncsu.edu/resolver/1840.16/5759.

MLA Handbook (7th Edition):

King, Rachel Marie. “On the Use of Wing Adaptation and Formation for Improved Aerodynamic Efficiency.” 2005. Web. 14 Nov 2019.

Vancouver:

King RM. On the Use of Wing Adaptation and Formation for Improved Aerodynamic Efficiency. [Internet] [Doctoral dissertation]. North Carolina State University; 2005. [cited 2019 Nov 14]. Available from: http://www.lib.ncsu.edu/resolver/1840.16/5759.

Council of Science Editors:

King RM. On the Use of Wing Adaptation and Formation for Improved Aerodynamic Efficiency. [Doctoral Dissertation]. North Carolina State University; 2005. Available from: http://www.lib.ncsu.edu/resolver/1840.16/5759


North Carolina State University

10. Jepson, Jeffrey Keith. Advancements in Aerodynamic Technologies for Airfoils and Wings.

Degree: PhD, Aerospace Engineering, 2006, North Carolina State University

 Although aircraft operate over a wide range of flight conditions, current fixed geometry aircraft are optimized for only a few of these conditions. By altering… (more)

Subjects/Keywords: Adaptive Aerodynamics; WIngs; Airfoils

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

APA (6th Edition):

Jepson, J. K. (2006). Advancements in Aerodynamic Technologies for Airfoils and Wings. (Doctoral Dissertation). North Carolina State University. Retrieved from http://www.lib.ncsu.edu/resolver/1840.16/5791

Chicago Manual of Style (16th Edition):

Jepson, Jeffrey Keith. “Advancements in Aerodynamic Technologies for Airfoils and Wings.” 2006. Doctoral Dissertation, North Carolina State University. Accessed November 14, 2019. http://www.lib.ncsu.edu/resolver/1840.16/5791.

MLA Handbook (7th Edition):

Jepson, Jeffrey Keith. “Advancements in Aerodynamic Technologies for Airfoils and Wings.” 2006. Web. 14 Nov 2019.

Vancouver:

Jepson JK. Advancements in Aerodynamic Technologies for Airfoils and Wings. [Internet] [Doctoral dissertation]. North Carolina State University; 2006. [cited 2019 Nov 14]. Available from: http://www.lib.ncsu.edu/resolver/1840.16/5791.

Council of Science Editors:

Jepson JK. Advancements in Aerodynamic Technologies for Airfoils and Wings. [Doctoral Dissertation]. North Carolina State University; 2006. Available from: http://www.lib.ncsu.edu/resolver/1840.16/5791


North Carolina State University

11. Shipley, Edward Nicholas Jr. Static Aeroelasticity Considerations in Aerodynamic Adaptation of Wings for Low Drag.

Degree: MS, Aerospace Engineering, 2006, North Carolina State University

 This thesis presents a methodology to calculate the flap angles necessary to reproduce a desired lift distribution for an elastic wing with multiple trailing-edge flaps.… (more)

Subjects/Keywords: adaptive wing; elliptic lift; profile drag; induced drag; aerodynamics; aeroelasticity

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

APA (6th Edition):

Shipley, E. N. J. (2006). Static Aeroelasticity Considerations in Aerodynamic Adaptation of Wings for Low Drag. (Thesis). North Carolina State University. Retrieved from http://www.lib.ncsu.edu/resolver/1840.16/1118

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Chicago Manual of Style (16th Edition):

Shipley, Edward Nicholas Jr. “Static Aeroelasticity Considerations in Aerodynamic Adaptation of Wings for Low Drag.” 2006. Thesis, North Carolina State University. Accessed November 14, 2019. http://www.lib.ncsu.edu/resolver/1840.16/1118.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

MLA Handbook (7th Edition):

Shipley, Edward Nicholas Jr. “Static Aeroelasticity Considerations in Aerodynamic Adaptation of Wings for Low Drag.” 2006. Web. 14 Nov 2019.

Vancouver:

Shipley ENJ. Static Aeroelasticity Considerations in Aerodynamic Adaptation of Wings for Low Drag. [Internet] [Thesis]. North Carolina State University; 2006. [cited 2019 Nov 14]. Available from: http://www.lib.ncsu.edu/resolver/1840.16/1118.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Council of Science Editors:

Shipley ENJ. Static Aeroelasticity Considerations in Aerodynamic Adaptation of Wings for Low Drag. [Thesis]. North Carolina State University; 2006. Available from: http://www.lib.ncsu.edu/resolver/1840.16/1118

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

.