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

University: Indian Institute of Science

You searched for subject:( wing camber ). Showing records 1 – 16 of 16 total matches.

Search Limiters

Last 2 Years | English Only

No search limiters apply to these results.

▼ Search Limiters


Indian Institute of Science

1. Mukherjee, Sujoy. Structural Modeling And Analysis Of Insect Scale Flapping Wing.

Degree: 2012, Indian Institute of Science

 Micro Air Vehicles (MAVs) are defined as a class of vehicles with their larger dimension not exceeding 15 cm and weighing 100 gm. The three… (more)

Subjects/Keywords: Flapping Wing; Micro Air Vehicles (MAVs); Calliphora Wing; Flapping Wings; Twisting Wing; Flapping Flight; Aeronautics

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Mukherjee, S. (2012). Structural Modeling And Analysis Of Insect Scale Flapping Wing. (Thesis). Indian Institute of Science. Retrieved from http://hdl.handle.net/2005/2021

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):

Mukherjee, Sujoy. “Structural Modeling And Analysis Of Insect Scale Flapping Wing.” 2012. Thesis, Indian Institute of Science. Accessed September 18, 2019. http://hdl.handle.net/2005/2021.

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

MLA Handbook (7th Edition):

Mukherjee, Sujoy. “Structural Modeling And Analysis Of Insect Scale Flapping Wing.” 2012. Web. 18 Sep 2019.

Vancouver:

Mukherjee S. Structural Modeling And Analysis Of Insect Scale Flapping Wing. [Internet] [Thesis]. Indian Institute of Science; 2012. [cited 2019 Sep 18]. Available from: http://hdl.handle.net/2005/2021.

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

Council of Science Editors:

Mukherjee S. Structural Modeling And Analysis Of Insect Scale Flapping Wing. [Thesis]. Indian Institute of Science; 2012. Available from: http://hdl.handle.net/2005/2021

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


Indian Institute of Science

2. Mukherjee, Sujoy. Structural Modeling And Analysis Of Insect Scale Flapping Wing.

Degree: 2012, Indian Institute of Science

 Micro Air Vehicles (MAVs) are defined as a class of vehicles with their larger dimension not exceeding 15 cm and weighing 100 gm. The three… (more)

Subjects/Keywords: Flapping Wing; Micro Air Vehicles (MAVs); Calliphora Wing; Flapping Wings; Twisting Wing; Flapping Flight; Aeronautics

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Mukherjee, S. (2012). Structural Modeling And Analysis Of Insect Scale Flapping Wing. (Thesis). Indian Institute of Science. Retrieved from http://etd.iisc.ernet.in/handle/2005/2021 ; http://etd.ncsi.iisc.ernet.in/abstracts/2616/G24985-Abs.pdf

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):

Mukherjee, Sujoy. “Structural Modeling And Analysis Of Insect Scale Flapping Wing.” 2012. Thesis, Indian Institute of Science. Accessed September 18, 2019. http://etd.iisc.ernet.in/handle/2005/2021 ; http://etd.ncsi.iisc.ernet.in/abstracts/2616/G24985-Abs.pdf.

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

MLA Handbook (7th Edition):

Mukherjee, Sujoy. “Structural Modeling And Analysis Of Insect Scale Flapping Wing.” 2012. Web. 18 Sep 2019.

Vancouver:

Mukherjee S. Structural Modeling And Analysis Of Insect Scale Flapping Wing. [Internet] [Thesis]. Indian Institute of Science; 2012. [cited 2019 Sep 18]. Available from: http://etd.iisc.ernet.in/handle/2005/2021 ; http://etd.ncsi.iisc.ernet.in/abstracts/2616/G24985-Abs.pdf.

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

Council of Science Editors:

Mukherjee S. Structural Modeling And Analysis Of Insect Scale Flapping Wing. [Thesis]. Indian Institute of Science; 2012. Available from: http://etd.iisc.ernet.in/handle/2005/2021 ; http://etd.ncsi.iisc.ernet.in/abstracts/2616/G24985-Abs.pdf

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


Indian Institute of Science

3. Mysa, Ravi Chaithanya. Fluid-Elastic Interactions in Flutter And Flapping Wing Propulsion.

Degree: 2013, Indian Institute of Science

 This study seeks to understand the interplay of vorticity and elasto-dynamics that forms the basis for a fluttering flag and flapping wing propulsion, and factors… (more)

Subjects/Keywords: Wing Propulsion; Flapping Wing Propulsion; Fluttering Wing Propulsion; Fluttering Flags; Flapping Foils; Wing Propulsion Vorticity; Wing Propulsion Elasto-Dynamics; Viscous Fluid Flow; Flexible Foil; Aerospace Engineering

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Mysa, R. C. (2013). Fluid-Elastic Interactions in Flutter And Flapping Wing Propulsion. (Thesis). Indian Institute of Science. Retrieved from http://hdl.handle.net/2005/2706

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):

Mysa, Ravi Chaithanya. “Fluid-Elastic Interactions in Flutter And Flapping Wing Propulsion.” 2013. Thesis, Indian Institute of Science. Accessed September 18, 2019. http://hdl.handle.net/2005/2706.

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

MLA Handbook (7th Edition):

Mysa, Ravi Chaithanya. “Fluid-Elastic Interactions in Flutter And Flapping Wing Propulsion.” 2013. Web. 18 Sep 2019.

Vancouver:

Mysa RC. Fluid-Elastic Interactions in Flutter And Flapping Wing Propulsion. [Internet] [Thesis]. Indian Institute of Science; 2013. [cited 2019 Sep 18]. Available from: http://hdl.handle.net/2005/2706.

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

Council of Science Editors:

Mysa RC. Fluid-Elastic Interactions in Flutter And Flapping Wing Propulsion. [Thesis]. Indian Institute of Science; 2013. Available from: http://hdl.handle.net/2005/2706

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


Indian Institute of Science

4. Mysa, Ravi Chaithanya. Fluid-Elastic Interactions in Flutter And Flapping Wing Propulsion.

Degree: 2013, Indian Institute of Science

 This study seeks to understand the interplay of vorticity and elasto-dynamics that forms the basis for a fluttering flag and flapping wing propulsion, and factors… (more)

Subjects/Keywords: Wing Propulsion; Flapping Wing Propulsion; Fluttering Wing Propulsion; Fluttering Flags; Flapping Foils; Wing Propulsion Vorticity; Wing Propulsion Elasto-Dynamics; Viscous Fluid Flow; Flexible Foil; Aerospace Engineering

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Mysa, R. C. (2013). Fluid-Elastic Interactions in Flutter And Flapping Wing Propulsion. (Thesis). Indian Institute of Science. Retrieved from http://etd.iisc.ernet.in/handle/2005/2706 ; http://etd.ncsi.iisc.ernet.in/abstracts/3529/G26380-Abs.pdf

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):

Mysa, Ravi Chaithanya. “Fluid-Elastic Interactions in Flutter And Flapping Wing Propulsion.” 2013. Thesis, Indian Institute of Science. Accessed September 18, 2019. http://etd.iisc.ernet.in/handle/2005/2706 ; http://etd.ncsi.iisc.ernet.in/abstracts/3529/G26380-Abs.pdf.

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

MLA Handbook (7th Edition):

Mysa, Ravi Chaithanya. “Fluid-Elastic Interactions in Flutter And Flapping Wing Propulsion.” 2013. Web. 18 Sep 2019.

Vancouver:

Mysa RC. Fluid-Elastic Interactions in Flutter And Flapping Wing Propulsion. [Internet] [Thesis]. Indian Institute of Science; 2013. [cited 2019 Sep 18]. Available from: http://etd.iisc.ernet.in/handle/2005/2706 ; http://etd.ncsi.iisc.ernet.in/abstracts/3529/G26380-Abs.pdf.

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

Council of Science Editors:

Mysa RC. Fluid-Elastic Interactions in Flutter And Flapping Wing Propulsion. [Thesis]. Indian Institute of Science; 2013. Available from: http://etd.iisc.ernet.in/handle/2005/2706 ; http://etd.ncsi.iisc.ernet.in/abstracts/3529/G26380-Abs.pdf

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


Indian Institute of Science

5. Pushpangathan, Jinraj V. Design and Development of 75 mm Fixed-Wing Nano Air Vehicle.

Degree: 2017, Indian Institute of Science

 This thesis deals with the design and development of a 75 mm fixed-wing nano-air vehicle (NAV). The NAV is designed to fit inside a cube… (more)

Subjects/Keywords: Nano Air Vehicle (NAV); Flight Control System Design; Fixed Wing Nano Air Vehicle; 75 mm Fixed-Wing Nano Air Vehicle Design; Fixed-Wing Air Vehicle; Aerospace Engineering

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Pushpangathan, J. V. (2017). Design and Development of 75 mm Fixed-Wing Nano Air Vehicle. (Thesis). Indian Institute of Science. Retrieved from http://etd.iisc.ernet.in/2005/3689 ; http://etd.iisc.ernet.in/abstracts/4559/G28507-Abs.pdf

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):

Pushpangathan, Jinraj V. “Design and Development of 75 mm Fixed-Wing Nano Air Vehicle.” 2017. Thesis, Indian Institute of Science. Accessed September 18, 2019. http://etd.iisc.ernet.in/2005/3689 ; http://etd.iisc.ernet.in/abstracts/4559/G28507-Abs.pdf.

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

MLA Handbook (7th Edition):

Pushpangathan, Jinraj V. “Design and Development of 75 mm Fixed-Wing Nano Air Vehicle.” 2017. Web. 18 Sep 2019.

Vancouver:

Pushpangathan JV. Design and Development of 75 mm Fixed-Wing Nano Air Vehicle. [Internet] [Thesis]. Indian Institute of Science; 2017. [cited 2019 Sep 18]. Available from: http://etd.iisc.ernet.in/2005/3689 ; http://etd.iisc.ernet.in/abstracts/4559/G28507-Abs.pdf.

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

Council of Science Editors:

Pushpangathan JV. Design and Development of 75 mm Fixed-Wing Nano Air Vehicle. [Thesis]. Indian Institute of Science; 2017. Available from: http://etd.iisc.ernet.in/2005/3689 ; http://etd.iisc.ernet.in/abstracts/4559/G28507-Abs.pdf

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


Indian Institute of Science

6. Chattaraj, Nilanjan. A Design Procedure for Flapping Wings Comprising Piezoelectric Actuators, Driver Circuit, and a Compliant Mechanism.

Degree: 2015, Indian Institute of Science

 Flapping-wing micro air vehicle (MAV) is an emerging micro-robotic technology, which has several challenges toward its practical implementation. Inspired by insect flight, researchers have adopted… (more)

Subjects/Keywords: Flapping Wing Microair Vehicle; Microrobotic Technology; Piezoelectric Actuator; Compliant Flapping Mechanism; Flapping Wing MAV; Piezoelectric Bimorph Actuator; Piezoelectric Flapping Actuator; Piezo-Actuators; Flapping-Wing Micro Air Vehicles; Piezoelectric Bimorph; Piezo-actuated Flapping Wing; Aerospace Engineering

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Chattaraj, N. (2015). A Design Procedure for Flapping Wings Comprising Piezoelectric Actuators, Driver Circuit, and a Compliant Mechanism. (Thesis). Indian Institute of Science. Retrieved from http://etd.iisc.ernet.in/2005/3661 ; http://etd.iisc.ernet.in/abstracts/4531/G27313-Abs.pdf

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):

Chattaraj, Nilanjan. “A Design Procedure for Flapping Wings Comprising Piezoelectric Actuators, Driver Circuit, and a Compliant Mechanism.” 2015. Thesis, Indian Institute of Science. Accessed September 18, 2019. http://etd.iisc.ernet.in/2005/3661 ; http://etd.iisc.ernet.in/abstracts/4531/G27313-Abs.pdf.

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

MLA Handbook (7th Edition):

Chattaraj, Nilanjan. “A Design Procedure for Flapping Wings Comprising Piezoelectric Actuators, Driver Circuit, and a Compliant Mechanism.” 2015. Web. 18 Sep 2019.

Vancouver:

Chattaraj N. A Design Procedure for Flapping Wings Comprising Piezoelectric Actuators, Driver Circuit, and a Compliant Mechanism. [Internet] [Thesis]. Indian Institute of Science; 2015. [cited 2019 Sep 18]. Available from: http://etd.iisc.ernet.in/2005/3661 ; http://etd.iisc.ernet.in/abstracts/4531/G27313-Abs.pdf.

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

Council of Science Editors:

Chattaraj N. A Design Procedure for Flapping Wings Comprising Piezoelectric Actuators, Driver Circuit, and a Compliant Mechanism. [Thesis]. Indian Institute of Science; 2015. Available from: http://etd.iisc.ernet.in/2005/3661 ; http://etd.iisc.ernet.in/abstracts/4531/G27313-Abs.pdf

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


Indian Institute of Science

7. Marianandam, Peter Arun. Vision-based Strategies for Landing of Fixed Wing Unmanned Aerial Vehicles.

Degree: 2015, Indian Institute of Science

 Vision-based conventional landing of a fixed wing UAV is addressed in this thesis. The work includes mathematical modeling, interface to a software for rendering the… (more)

Subjects/Keywords: Computer Vision; Image Processing; Fixed Wing Unmanned Aerial Vehicles; Vision-in-the-Loop-Simulation (VILS); Vision Based Runway Alignment; Autonomous Landing Control; Vision Based Landing; Manned Fixed Wing Aircraft Landing Data; Cross Wind Landing; Vision-Based Landing; Vision-Based Cross Wind Landing; Fixed Wing UAVs; Aerospace Engineering

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Marianandam, P. A. (2015). Vision-based Strategies for Landing of Fixed Wing Unmanned Aerial Vehicles. (Thesis). Indian Institute of Science. Retrieved from http://etd.iisc.ernet.in/2005/3529 ; http://etd.iisc.ernet.in/abstracts/4397/G27582-Abs.pdf

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):

Marianandam, Peter Arun. “Vision-based Strategies for Landing of Fixed Wing Unmanned Aerial Vehicles.” 2015. Thesis, Indian Institute of Science. Accessed September 18, 2019. http://etd.iisc.ernet.in/2005/3529 ; http://etd.iisc.ernet.in/abstracts/4397/G27582-Abs.pdf.

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

MLA Handbook (7th Edition):

Marianandam, Peter Arun. “Vision-based Strategies for Landing of Fixed Wing Unmanned Aerial Vehicles.” 2015. Web. 18 Sep 2019.

Vancouver:

Marianandam PA. Vision-based Strategies for Landing of Fixed Wing Unmanned Aerial Vehicles. [Internet] [Thesis]. Indian Institute of Science; 2015. [cited 2019 Sep 18]. Available from: http://etd.iisc.ernet.in/2005/3529 ; http://etd.iisc.ernet.in/abstracts/4397/G27582-Abs.pdf.

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

Council of Science Editors:

Marianandam PA. Vision-based Strategies for Landing of Fixed Wing Unmanned Aerial Vehicles. [Thesis]. Indian Institute of Science; 2015. Available from: http://etd.iisc.ernet.in/2005/3529 ; http://etd.iisc.ernet.in/abstracts/4397/G27582-Abs.pdf

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


Indian Institute of Science

8. Agarwal, R K. Study Of Aerodynamic Effectiveness Of Wing Tip Sails For Gust Load Alleviation.

Degree: 2004, Indian Institute of Science

Subjects/Keywords: Aerodynamics; Wings - Load Alleviation; Load Alleviation; Wing Tip Sails; Gust Load Alleviation; Wing Tunnel Tests; Gust Loads; Vortex Lattlce Method; Aeronautics

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Agarwal, R. K. (2004). Study Of Aerodynamic Effectiveness Of Wing Tip Sails For Gust Load Alleviation. (Thesis). Indian Institute of Science. Retrieved from http://hdl.handle.net/2005/1139

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):

Agarwal, R K. “Study Of Aerodynamic Effectiveness Of Wing Tip Sails For Gust Load Alleviation.” 2004. Thesis, Indian Institute of Science. Accessed September 18, 2019. http://hdl.handle.net/2005/1139.

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

MLA Handbook (7th Edition):

Agarwal, R K. “Study Of Aerodynamic Effectiveness Of Wing Tip Sails For Gust Load Alleviation.” 2004. Web. 18 Sep 2019.

Vancouver:

Agarwal RK. Study Of Aerodynamic Effectiveness Of Wing Tip Sails For Gust Load Alleviation. [Internet] [Thesis]. Indian Institute of Science; 2004. [cited 2019 Sep 18]. Available from: http://hdl.handle.net/2005/1139.

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

Council of Science Editors:

Agarwal RK. Study Of Aerodynamic Effectiveness Of Wing Tip Sails For Gust Load Alleviation. [Thesis]. Indian Institute of Science; 2004. Available from: http://hdl.handle.net/2005/1139

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


Indian Institute of Science

9. Parween, Rizuwana. Modeling of the Haltere-A Natural Micro-Scale Vibratory Gyroscope.

Degree: 2015, Indian Institute of Science

 Vibratory gyroscopes have gained immense popularity in the microsystem technology because of their suitability to planar fabrication techniques. With considerable effort in design and fabrication,… (more)

Subjects/Keywords: Gyrosocopic Halteres; Micro Scale Visratory Gyrosocopic; Micro-Electro-Mechanical-System; Haltere's Boundary; Haltere’s Asymmetry; Wing-Haltere Coupled Model; Haltere's Modeling; Haltere’s Attachment; Wing-Haltere Mechanism; Soldier Fly Halteres; Crane Fly Haltere; Mechanical Engineering

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Parween, R. (2015). Modeling of the Haltere-A Natural Micro-Scale Vibratory Gyroscope. (Thesis). Indian Institute of Science. Retrieved from http://etd.iisc.ernet.in/2005/3655 ; http://etd.iisc.ernet.in/abstracts/4525/G27304-Abs.pdf

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):

Parween, Rizuwana. “Modeling of the Haltere-A Natural Micro-Scale Vibratory Gyroscope.” 2015. Thesis, Indian Institute of Science. Accessed September 18, 2019. http://etd.iisc.ernet.in/2005/3655 ; http://etd.iisc.ernet.in/abstracts/4525/G27304-Abs.pdf.

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

MLA Handbook (7th Edition):

Parween, Rizuwana. “Modeling of the Haltere-A Natural Micro-Scale Vibratory Gyroscope.” 2015. Web. 18 Sep 2019.

Vancouver:

Parween R. Modeling of the Haltere-A Natural Micro-Scale Vibratory Gyroscope. [Internet] [Thesis]. Indian Institute of Science; 2015. [cited 2019 Sep 18]. Available from: http://etd.iisc.ernet.in/2005/3655 ; http://etd.iisc.ernet.in/abstracts/4525/G27304-Abs.pdf.

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

Council of Science Editors:

Parween R. Modeling of the Haltere-A Natural Micro-Scale Vibratory Gyroscope. [Thesis]. Indian Institute of Science; 2015. Available from: http://etd.iisc.ernet.in/2005/3655 ; http://etd.iisc.ernet.in/abstracts/4525/G27304-Abs.pdf

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


Indian Institute of Science

10. Gopalakrishna, N. On Three Dimensional High Lift Flow Computations.

Degree: 2014, Indian Institute of Science

 Computing 3D high lift flows has been a challenge to the CFD community because of three important reasons: complex physics, complex geometries and large computational… (more)

Subjects/Keywords: High Lift Flow; Trap Wing; Aerodynamic Design; Fluid Mechanics; Computational Fluid Dynamics (CFD); High Resolution Flow Solver for UNstructured Meshes; Grid Generation; Turbulence; Trapezoidal Wing; 3D High Lift Flow; High Lift Flow Computations; HiFUN; HiFUN Solver; Aerospace Engineering

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Gopalakrishna, N. (2014). On Three Dimensional High Lift Flow Computations. (Thesis). Indian Institute of Science. Retrieved from http://hdl.handle.net/2005/3127

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):

Gopalakrishna, N. “On Three Dimensional High Lift Flow Computations.” 2014. Thesis, Indian Institute of Science. Accessed September 18, 2019. http://hdl.handle.net/2005/3127.

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

MLA Handbook (7th Edition):

Gopalakrishna, N. “On Three Dimensional High Lift Flow Computations.” 2014. Web. 18 Sep 2019.

Vancouver:

Gopalakrishna N. On Three Dimensional High Lift Flow Computations. [Internet] [Thesis]. Indian Institute of Science; 2014. [cited 2019 Sep 18]. Available from: http://hdl.handle.net/2005/3127.

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

Council of Science Editors:

Gopalakrishna N. On Three Dimensional High Lift Flow Computations. [Thesis]. Indian Institute of Science; 2014. Available from: http://hdl.handle.net/2005/3127

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


Indian Institute of Science

11. Nathan, Vinay. Analysis of Unsteady Incompressible Potential Flow Over a Swimming Slender Fish and a Swept Wing Tail.

Degree: 2015, Indian Institute of Science

 This thesis deals with computing the pressure distribution around a swimming slender fish and the thrust generated by its flapping motion. The body of the… (more)

Subjects/Keywords: Swimming Slender Fish Flow Dynamics; Slender Body Flow Model; Swept Wing Model; Planar Wing Flow; Unsteady Flows; Vortex Dynamics; Swimming Propulsion; Unsteady Propulsion; Fishlike Swimmimg Hydrodynamics; Fish Near-Body Flow Dynamics; Marine Propulsion; Fluid Dynamics; Vortex Panel Method; Bernoulli Equation; Aerospace Engineering

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Nathan, V. (2015). Analysis of Unsteady Incompressible Potential Flow Over a Swimming Slender Fish and a Swept Wing Tail. (Thesis). Indian Institute of Science. Retrieved from http://etd.iisc.ernet.in/2005/3551 ; http://etd.iisc.ernet.in/abstracts/4419/G27333-Abs.pdf

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):

Nathan, Vinay. “Analysis of Unsteady Incompressible Potential Flow Over a Swimming Slender Fish and a Swept Wing Tail.” 2015. Thesis, Indian Institute of Science. Accessed September 18, 2019. http://etd.iisc.ernet.in/2005/3551 ; http://etd.iisc.ernet.in/abstracts/4419/G27333-Abs.pdf.

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

MLA Handbook (7th Edition):

Nathan, Vinay. “Analysis of Unsteady Incompressible Potential Flow Over a Swimming Slender Fish and a Swept Wing Tail.” 2015. Web. 18 Sep 2019.

Vancouver:

Nathan V. Analysis of Unsteady Incompressible Potential Flow Over a Swimming Slender Fish and a Swept Wing Tail. [Internet] [Thesis]. Indian Institute of Science; 2015. [cited 2019 Sep 18]. Available from: http://etd.iisc.ernet.in/2005/3551 ; http://etd.iisc.ernet.in/abstracts/4419/G27333-Abs.pdf.

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

Council of Science Editors:

Nathan V. Analysis of Unsteady Incompressible Potential Flow Over a Swimming Slender Fish and a Swept Wing Tail. [Thesis]. Indian Institute of Science; 2015. Available from: http://etd.iisc.ernet.in/2005/3551 ; http://etd.iisc.ernet.in/abstracts/4419/G27333-Abs.pdf

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


Indian Institute of Science

12. Bera, Titas. Application of Randomized Algorithms in Path Planning and Control of a Micro Air Vehicle.

Degree: 2015, Indian Institute of Science

 This thesis focuses on the design and development of a fixed wing micro air vehicle (MAV) and on the development of randomized sampling based motion… (more)

Subjects/Keywords: Micro Air Vehicles; Fixed Wing Micro Air Vehicles; Aerodynamic Design; Computational Fluid Dynamics; Probabilistic Robust Control; Randomized Motion Planning; Narrow Passage Sampling; Rapidly Exploring Random Tree; Low Reynolds Number Aerodynamics; Fixed Wing MAVs; Micro Air Vehicle Design; Narrow Passage Sampling Algorithms; Geometric Probability; Aerospace Engineering

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Bera, T. (2015). Application of Randomized Algorithms in Path Planning and Control of a Micro Air Vehicle. (Thesis). Indian Institute of Science. Retrieved from http://etd.iisc.ernet.in/2005/3756 ; http://etd.iisc.ernet.in/abstracts/4627/G26957-Abs.pdf

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):

Bera, Titas. “Application of Randomized Algorithms in Path Planning and Control of a Micro Air Vehicle.” 2015. Thesis, Indian Institute of Science. Accessed September 18, 2019. http://etd.iisc.ernet.in/2005/3756 ; http://etd.iisc.ernet.in/abstracts/4627/G26957-Abs.pdf.

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

MLA Handbook (7th Edition):

Bera, Titas. “Application of Randomized Algorithms in Path Planning and Control of a Micro Air Vehicle.” 2015. Web. 18 Sep 2019.

Vancouver:

Bera T. Application of Randomized Algorithms in Path Planning and Control of a Micro Air Vehicle. [Internet] [Thesis]. Indian Institute of Science; 2015. [cited 2019 Sep 18]. Available from: http://etd.iisc.ernet.in/2005/3756 ; http://etd.iisc.ernet.in/abstracts/4627/G26957-Abs.pdf.

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

Council of Science Editors:

Bera T. Application of Randomized Algorithms in Path Planning and Control of a Micro Air Vehicle. [Thesis]. Indian Institute of Science; 2015. Available from: http://etd.iisc.ernet.in/2005/3756 ; http://etd.iisc.ernet.in/abstracts/4627/G26957-Abs.pdf

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


Indian Institute of Science

13. Rai, Mamta. Spatio-Temporal Control Of Drosophila Indirect Flight Muscle Development And Maintenance By The Transcription Factor Erect Wing.

Degree: 2012, Indian Institute of Science

 Muscle development involves concerted action of a repertoire of mechanisms governing myoblast proliferation, migration, fusion and differentiation. Subsequently, there are cellular events administrating proper muscle… (more)

Subjects/Keywords: Drosophila melanogaster; Drosophila; Vertebrates - Skeletal Muscle Development; Myofibrillogenesis; Myoblasts; Myogenesis; Myoblast Fusion; Erect Wing (EWG); Mitorchondrial Fusion; Indirect Flight Muscle Development; Drosophila Muscle Development; Indirect Flight Muscle Patterning; Muscle Pattern; Muscle Mutants; Myonuclear Number; Developmental Biology

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Rai, M. (2012). Spatio-Temporal Control Of Drosophila Indirect Flight Muscle Development And Maintenance By The Transcription Factor Erect Wing. (Thesis). Indian Institute of Science. Retrieved from http://etd.iisc.ernet.in/handle/2005/2525 ; http://etd.ncsi.iisc.ernet.in/abstracts/3276/G25562-Abs.pdf

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):

Rai, Mamta. “Spatio-Temporal Control Of Drosophila Indirect Flight Muscle Development And Maintenance By The Transcription Factor Erect Wing.” 2012. Thesis, Indian Institute of Science. Accessed September 18, 2019. http://etd.iisc.ernet.in/handle/2005/2525 ; http://etd.ncsi.iisc.ernet.in/abstracts/3276/G25562-Abs.pdf.

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

MLA Handbook (7th Edition):

Rai, Mamta. “Spatio-Temporal Control Of Drosophila Indirect Flight Muscle Development And Maintenance By The Transcription Factor Erect Wing.” 2012. Web. 18 Sep 2019.

Vancouver:

Rai M. Spatio-Temporal Control Of Drosophila Indirect Flight Muscle Development And Maintenance By The Transcription Factor Erect Wing. [Internet] [Thesis]. Indian Institute of Science; 2012. [cited 2019 Sep 18]. Available from: http://etd.iisc.ernet.in/handle/2005/2525 ; http://etd.ncsi.iisc.ernet.in/abstracts/3276/G25562-Abs.pdf.

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

Council of Science Editors:

Rai M. Spatio-Temporal Control Of Drosophila Indirect Flight Muscle Development And Maintenance By The Transcription Factor Erect Wing. [Thesis]. Indian Institute of Science; 2012. Available from: http://etd.iisc.ernet.in/handle/2005/2525 ; http://etd.ncsi.iisc.ernet.in/abstracts/3276/G25562-Abs.pdf

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


Indian Institute of Science

14. Mondal, Partha. Wing in Ground Effect.

Degree: 2013, Indian Institute of Science

 The thesis presents a two pronged approach for predicting aerodynamics of air- foils/wings in the vicinity of the ground. The first approach is effectively a… (more)

Subjects/Keywords: Ground Effect; Ground-Cushion Phenomenon; Airfoils; Wings; Kutta-Joukowski Theorem; Discrete Vortex Method; 3D Ground Effect Model; Computational Fluid Dynamics; Aerodynamics; Dynamic Ground Effect Analysis; Sinking Grid Methodology; Flow Solver; Inverted Ground Effect Wing; Dynamic Ground Approach; Ground Effect Studies; Aerospace Engineering

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Mondal, P. (2013). Wing in Ground Effect. (Thesis). Indian Institute of Science. Retrieved from http://etd.iisc.ernet.in/handle/2005/2848 ; http://etd.ncsi.iisc.ernet.in/abstracts/3700/G26283(Abs).pdf

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):

Mondal, Partha. “Wing in Ground Effect.” 2013. Thesis, Indian Institute of Science. Accessed September 18, 2019. http://etd.iisc.ernet.in/handle/2005/2848 ; http://etd.ncsi.iisc.ernet.in/abstracts/3700/G26283(Abs).pdf.

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

MLA Handbook (7th Edition):

Mondal, Partha. “Wing in Ground Effect.” 2013. Web. 18 Sep 2019.

Vancouver:

Mondal P. Wing in Ground Effect. [Internet] [Thesis]. Indian Institute of Science; 2013. [cited 2019 Sep 18]. Available from: http://etd.iisc.ernet.in/handle/2005/2848 ; http://etd.ncsi.iisc.ernet.in/abstracts/3700/G26283(Abs).pdf.

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

Council of Science Editors:

Mondal P. Wing in Ground Effect. [Thesis]. Indian Institute of Science; 2013. Available from: http://etd.iisc.ernet.in/handle/2005/2848 ; http://etd.ncsi.iisc.ernet.in/abstracts/3700/G26283(Abs).pdf

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


Indian Institute of Science

15. Rai, Mamta. Spatio-Temporal Control Of Drosophila Indirect Flight Muscle Development And Maintenance By The Transcription Factor Erect Wing.

Degree: 2012, Indian Institute of Science

 Muscle development involves concerted action of a repertoire of mechanisms governing myoblast proliferation, migration, fusion and differentiation. Subsequently, there are cellular events administrating proper muscle… (more)

Subjects/Keywords: Drosophila melanogaster; Drosophila; Vertebrates - Skeletal Muscle Development; Myofibrillogenesis; Myoblasts; Myogenesis; Myoblast Fusion; Erect Wing (EWG); Mitorchondrial Fusion; Indirect Flight Muscle Development; Drosophila Muscle Development; Indirect Flight Muscle Patterning; Muscle Pattern; Muscle Mutants; Myonuclear Number; Developmental Biology

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Rai, M. (2012). Spatio-Temporal Control Of Drosophila Indirect Flight Muscle Development And Maintenance By The Transcription Factor Erect Wing. (Thesis). Indian Institute of Science. Retrieved from http://hdl.handle.net/2005/2525

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):

Rai, Mamta. “Spatio-Temporal Control Of Drosophila Indirect Flight Muscle Development And Maintenance By The Transcription Factor Erect Wing.” 2012. Thesis, Indian Institute of Science. Accessed September 18, 2019. http://hdl.handle.net/2005/2525.

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

MLA Handbook (7th Edition):

Rai, Mamta. “Spatio-Temporal Control Of Drosophila Indirect Flight Muscle Development And Maintenance By The Transcription Factor Erect Wing.” 2012. Web. 18 Sep 2019.

Vancouver:

Rai M. Spatio-Temporal Control Of Drosophila Indirect Flight Muscle Development And Maintenance By The Transcription Factor Erect Wing. [Internet] [Thesis]. Indian Institute of Science; 2012. [cited 2019 Sep 18]. Available from: http://hdl.handle.net/2005/2525.

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

Council of Science Editors:

Rai M. Spatio-Temporal Control Of Drosophila Indirect Flight Muscle Development And Maintenance By The Transcription Factor Erect Wing. [Thesis]. Indian Institute of Science; 2012. Available from: http://hdl.handle.net/2005/2525

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


Indian Institute of Science

16. Mondal, Partha. Wing in Ground Effect.

Degree: 2013, Indian Institute of Science

 The thesis presents a two pronged approach for predicting aerodynamics of air- foils/wings in the vicinity of the ground. The first approach is effectively a… (more)

Subjects/Keywords: Ground Effect; Ground-Cushion Phenomenon; Airfoils; Wings; Kutta-Joukowski Theorem; Discrete Vortex Method; 3D Ground Effect Model; Computational Fluid Dynamics; Aerodynamics; Dynamic Ground Effect Analysis; Sinking Grid Methodology; Flow Solver; Inverted Ground Effect Wing; Dynamic Ground Approach; Ground Effect Studies; Aerospace Engineering

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Mondal, P. (2013). Wing in Ground Effect. (Thesis). Indian Institute of Science. Retrieved from http://hdl.handle.net/2005/2848

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):

Mondal, Partha. “Wing in Ground Effect.” 2013. Thesis, Indian Institute of Science. Accessed September 18, 2019. http://hdl.handle.net/2005/2848.

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

MLA Handbook (7th Edition):

Mondal, Partha. “Wing in Ground Effect.” 2013. Web. 18 Sep 2019.

Vancouver:

Mondal P. Wing in Ground Effect. [Internet] [Thesis]. Indian Institute of Science; 2013. [cited 2019 Sep 18]. Available from: http://hdl.handle.net/2005/2848.

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

Council of Science Editors:

Mondal P. Wing in Ground Effect. [Thesis]. Indian Institute of Science; 2013. Available from: http://hdl.handle.net/2005/2848

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

.