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 subject:(Tailless aircraft). Showing records 1 – 10 of 10 total matches.

Search Limiters

Last 2 Years | English Only

No search limiters apply to these results.

▼ Search Limiters


Delft University of Technology

1. Stolk, Rob (author). Minimum drag control allocation for the Innovative Control Effector aircraft: Optimal use of control redundancy on modern fighters.

Degree: 2017, Delft University of Technology

The Innovative Control Effector model is a tailless delta-wing aircraft concept equipped with 11 control surfaces with overlapping functionality and two-directional thrust vectoring. The high… (more)

Subjects/Keywords: Control Allocation; Innovative Control Effectors; ICE; Incremental Control; Tailless Aircraft; Drag

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Stolk, R. (. (2017). Minimum drag control allocation for the Innovative Control Effector aircraft: Optimal use of control redundancy on modern fighters. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:43ce35bc-eb94-4c7b-a826-80a80e24a6d6

Chicago Manual of Style (16th Edition):

Stolk, Rob (author). “Minimum drag control allocation for the Innovative Control Effector aircraft: Optimal use of control redundancy on modern fighters.” 2017. Masters Thesis, Delft University of Technology. Accessed January 18, 2021. http://resolver.tudelft.nl/uuid:43ce35bc-eb94-4c7b-a826-80a80e24a6d6.

MLA Handbook (7th Edition):

Stolk, Rob (author). “Minimum drag control allocation for the Innovative Control Effector aircraft: Optimal use of control redundancy on modern fighters.” 2017. Web. 18 Jan 2021.

Vancouver:

Stolk R(. Minimum drag control allocation for the Innovative Control Effector aircraft: Optimal use of control redundancy on modern fighters. [Internet] [Masters thesis]. Delft University of Technology; 2017. [cited 2021 Jan 18]. Available from: http://resolver.tudelft.nl/uuid:43ce35bc-eb94-4c7b-a826-80a80e24a6d6.

Council of Science Editors:

Stolk R(. Minimum drag control allocation for the Innovative Control Effector aircraft: Optimal use of control redundancy on modern fighters. [Masters Thesis]. Delft University of Technology; 2017. Available from: http://resolver.tudelft.nl/uuid:43ce35bc-eb94-4c7b-a826-80a80e24a6d6


University of Missouri – Kansas City

2. Kraft, Tyler E. Extended Range Tactical Resupply Using Tailless UAV.

Degree: 2017, University of Missouri – Kansas City

 An alternative approach for precision aerial delivery utilizing a flying wing for controllable forward glide is presented. Although effective, current delivery methods either display a… (more)

Subjects/Keywords: Thesis  – University of Missouri – Kansas City  – Engineering; Delivery of goods; Drone aircraft; Airplanes, Tailless

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Kraft, T. E. (2017). Extended Range Tactical Resupply Using Tailless UAV. (Thesis). University of Missouri – Kansas City. Retrieved from http://hdl.handle.net/10355/62665

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):

Kraft, Tyler E. “Extended Range Tactical Resupply Using Tailless UAV.” 2017. Thesis, University of Missouri – Kansas City. Accessed January 18, 2021. http://hdl.handle.net/10355/62665.

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

MLA Handbook (7th Edition):

Kraft, Tyler E. “Extended Range Tactical Resupply Using Tailless UAV.” 2017. Web. 18 Jan 2021.

Vancouver:

Kraft TE. Extended Range Tactical Resupply Using Tailless UAV. [Internet] [Thesis]. University of Missouri – Kansas City; 2017. [cited 2021 Jan 18]. Available from: http://hdl.handle.net/10355/62665.

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

Council of Science Editors:

Kraft TE. Extended Range Tactical Resupply Using Tailless UAV. [Thesis]. University of Missouri – Kansas City; 2017. Available from: http://hdl.handle.net/10355/62665

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


Cranfield University

3. de Castro, Helena V. Flying and handling qualities of a fly-by-wire blended-wing-body civil transport aircraft.

Degree: PhD, School of Engineering, 2003, Cranfield University

 The blended-wing-body (BWB) configuration appears as a promising contender for the next generation of large transport aircraft. The idea of blending the wing with the… (more)

Subjects/Keywords: Tailless aircraft; Aircraft handling; Blended wing body; Fly by wire; Aircraft stability

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

de Castro, H. V. (2003). Flying and handling qualities of a fly-by-wire blended-wing-body civil transport aircraft. (Doctoral Dissertation). Cranfield University. Retrieved from http://hdl.handle.net/1826/119

Chicago Manual of Style (16th Edition):

de Castro, Helena V. “Flying and handling qualities of a fly-by-wire blended-wing-body civil transport aircraft.” 2003. Doctoral Dissertation, Cranfield University. Accessed January 18, 2021. http://hdl.handle.net/1826/119.

MLA Handbook (7th Edition):

de Castro, Helena V. “Flying and handling qualities of a fly-by-wire blended-wing-body civil transport aircraft.” 2003. Web. 18 Jan 2021.

Vancouver:

de Castro HV. Flying and handling qualities of a fly-by-wire blended-wing-body civil transport aircraft. [Internet] [Doctoral dissertation]. Cranfield University; 2003. [cited 2021 Jan 18]. Available from: http://hdl.handle.net/1826/119.

Council of Science Editors:

de Castro HV. Flying and handling qualities of a fly-by-wire blended-wing-body civil transport aircraft. [Doctoral Dissertation]. Cranfield University; 2003. Available from: http://hdl.handle.net/1826/119


Cranfield University

4. de Castro, Helena V. Flying and handling qualities of a fly-by-wire blended-wing-body civil transport aircraft.

Degree: PhD, 2003, Cranfield University

 The blended-wing-body (BWB) configuration appears as a promising contender for the next generation of large transport aircraft. The idea of blending the wing with the… (more)

Subjects/Keywords: 629.133340423; Tailless aircraft; Aircraft handling; Blended wing body; Fly by wire; Aircraft stability

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

de Castro, H. V. (2003). Flying and handling qualities of a fly-by-wire blended-wing-body civil transport aircraft. (Doctoral Dissertation). Cranfield University. Retrieved from http://dspace.lib.cranfield.ac.uk/handle/1826/119 ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.484641

Chicago Manual of Style (16th Edition):

de Castro, Helena V. “Flying and handling qualities of a fly-by-wire blended-wing-body civil transport aircraft.” 2003. Doctoral Dissertation, Cranfield University. Accessed January 18, 2021. http://dspace.lib.cranfield.ac.uk/handle/1826/119 ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.484641.

MLA Handbook (7th Edition):

de Castro, Helena V. “Flying and handling qualities of a fly-by-wire blended-wing-body civil transport aircraft.” 2003. Web. 18 Jan 2021.

Vancouver:

de Castro HV. Flying and handling qualities of a fly-by-wire blended-wing-body civil transport aircraft. [Internet] [Doctoral dissertation]. Cranfield University; 2003. [cited 2021 Jan 18]. Available from: http://dspace.lib.cranfield.ac.uk/handle/1826/119 ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.484641.

Council of Science Editors:

de Castro HV. Flying and handling qualities of a fly-by-wire blended-wing-body civil transport aircraft. [Doctoral Dissertation]. Cranfield University; 2003. Available from: http://dspace.lib.cranfield.ac.uk/handle/1826/119 ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.484641


North Carolina State University

5. 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

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

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 January 18, 2021. 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. 18 Jan 2021.

Vancouver:

Cusher AA. Ideal Lift Distributions and Flap Settings for Adaptive Tailless Aircraft. [Internet] [Thesis]. North Carolina State University; 2006. [cited 2021 Jan 18]. 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


Brno University of Technology

6. Prokop, Vít. Vývoj a vlastnosti bezocasých letadel: Evolution and Characteristics of Tailess Aircraft.

Degree: 2018, Brno University of Technology

 This bachelor work is about Evolution and Characteristics of Tailless Aircraft divided into two sections. The first section will cover the questions about stability and… (more)

Subjects/Keywords: Horten; Fauvel; Lippisch; Marske; SWIFT; samokřídlo; bezocasé letadlo; závěsný kluzák; profil; zkroucení křídla; stabilita; Horten; Fauvel; Lippisch; Marske; SWIFT; allwing aircraft; tailless aircraft; hangglider; airfoil; twisted wing; stability

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Prokop, V. (2018). Vývoj a vlastnosti bezocasých letadel: Evolution and Characteristics of Tailess Aircraft. (Thesis). Brno University of Technology. Retrieved from http://hdl.handle.net/11012/1703

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):

Prokop, Vít. “Vývoj a vlastnosti bezocasých letadel: Evolution and Characteristics of Tailess Aircraft.” 2018. Thesis, Brno University of Technology. Accessed January 18, 2021. http://hdl.handle.net/11012/1703.

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

MLA Handbook (7th Edition):

Prokop, Vít. “Vývoj a vlastnosti bezocasých letadel: Evolution and Characteristics of Tailess Aircraft.” 2018. Web. 18 Jan 2021.

Vancouver:

Prokop V. Vývoj a vlastnosti bezocasých letadel: Evolution and Characteristics of Tailess Aircraft. [Internet] [Thesis]. Brno University of Technology; 2018. [cited 2021 Jan 18]. Available from: http://hdl.handle.net/11012/1703.

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

Council of Science Editors:

Prokop V. Vývoj a vlastnosti bezocasých letadel: Evolution and Characteristics of Tailess Aircraft. [Thesis]. Brno University of Technology; 2018. Available from: http://hdl.handle.net/11012/1703

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

7. Langston, Sarah. Low-Speed Stability and Control of Exploratory Tailless Long-Range Supersonic Configurations.

Degree: 2015, University of Washington

 This thesis presents studies of the low-speed stability and control of a representative long-range supersonic flight vehicle. The aircraft of interest is a research uninhabited… (more)

Subjects/Keywords: Aircraft; Supersonic; Tailless; Aerospace engineering; aeronautics and astronautics

…8.3 Root Locus Plot of the Lat-Dir Tailless R-UAV Poles at Various Yaw and Roll Damper Gains… …8.4 Time History of Damper Augmented Tailless R-UAV to a 1 Degree Sideslip Angle… …8.5 Root Locus Plot of the Lat-Dir Tailless R-UAV Poles at Various Yaw and Roll Damper Gains… …8.6 Time History of Damper Augmented Tailless R-UAV to a 1 Degree Sideslip Angle… …8.9 Control Surface Responses Required to Stabilize Tailless R-UAV from the above State… 

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Langston, S. (2015). Low-Speed Stability and Control of Exploratory Tailless Long-Range Supersonic Configurations. (Thesis). University of Washington. Retrieved from http://hdl.handle.net/1773/33542

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):

Langston, Sarah. “Low-Speed Stability and Control of Exploratory Tailless Long-Range Supersonic Configurations.” 2015. Thesis, University of Washington. Accessed January 18, 2021. http://hdl.handle.net/1773/33542.

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

MLA Handbook (7th Edition):

Langston, Sarah. “Low-Speed Stability and Control of Exploratory Tailless Long-Range Supersonic Configurations.” 2015. Web. 18 Jan 2021.

Vancouver:

Langston S. Low-Speed Stability and Control of Exploratory Tailless Long-Range Supersonic Configurations. [Internet] [Thesis]. University of Washington; 2015. [cited 2021 Jan 18]. Available from: http://hdl.handle.net/1773/33542.

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

Council of Science Editors:

Langston S. Low-Speed Stability and Control of Exploratory Tailless Long-Range Supersonic Configurations. [Thesis]. University of Washington; 2015. Available from: http://hdl.handle.net/1773/33542

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


University of Pretoria

8. [No author]. Longitudinal handling characteristics of a tailless gull-wing aircraft .

Degree: 2008, University of Pretoria

 A handling quality investigation was performed on the swept gull-wing configuration. The swept gull-wing configuration is tailless and has a wing with a transition in… (more)

Subjects/Keywords: Flight simulation; Tumbling; Thumbprint criterion; Neal-smith analysis; C-star criterion; Shomber-gertsen analysis; Pilot induced oscillation; Oswald efficiency; Pilot mathematical model; Variable sweep wing; Exulans; Variable static margin; Swept gull-wing configuration; O-point; E-point; Handling qualities; Gust handling qualities; Tailless aircraft; Pecking; Monnich and dalldorff criterion; UCTD

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

author], [. (2008). Longitudinal handling characteristics of a tailless gull-wing aircraft . (Masters Thesis). University of Pretoria. Retrieved from http://upetd.up.ac.za/thesis/available/etd-09182008-132941/

Chicago Manual of Style (16th Edition):

author], [No. “Longitudinal handling characteristics of a tailless gull-wing aircraft .” 2008. Masters Thesis, University of Pretoria. Accessed January 18, 2021. http://upetd.up.ac.za/thesis/available/etd-09182008-132941/.

MLA Handbook (7th Edition):

author], [No. “Longitudinal handling characteristics of a tailless gull-wing aircraft .” 2008. Web. 18 Jan 2021.

Vancouver:

author] [. Longitudinal handling characteristics of a tailless gull-wing aircraft . [Internet] [Masters thesis]. University of Pretoria; 2008. [cited 2021 Jan 18]. Available from: http://upetd.up.ac.za/thesis/available/etd-09182008-132941/.

Council of Science Editors:

author] [. Longitudinal handling characteristics of a tailless gull-wing aircraft . [Masters Thesis]. University of Pretoria; 2008. Available from: http://upetd.up.ac.za/thesis/available/etd-09182008-132941/


University of Pretoria

9. Agenbag, Daniel Sarel. Longitudinal handling characteristics of a tailless gull-wing aircraft.

Degree: Mechanical and Aeronautical Engineering, 2008, University of Pretoria

 A handling quality investigation was performed on the swept gull-wing configuration. The swept gull-wing configuration is tailless and has a wing with a transition in… (more)

Subjects/Keywords: Flight simulation; Tumbling; Thumbprint criterion; Neal-smith analysis; C-star criterion; Shomber-gertsen analysis; Pilot induced oscillation; Oswald efficiency; Pilot mathematical model; Variable sweep wing; Exulans; Variable static margin; Swept gull-wing configuration; O-point; E-point; Handling qualities; Gust handling qualities; Tailless aircraft; Pecking; Monnich and dalldorff criterion; UCTD

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Agenbag, D. (2008). Longitudinal handling characteristics of a tailless gull-wing aircraft. (Masters Thesis). University of Pretoria. Retrieved from http://hdl.handle.net/2263/28011

Chicago Manual of Style (16th Edition):

Agenbag, Daniel. “Longitudinal handling characteristics of a tailless gull-wing aircraft.” 2008. Masters Thesis, University of Pretoria. Accessed January 18, 2021. http://hdl.handle.net/2263/28011.

MLA Handbook (7th Edition):

Agenbag, Daniel. “Longitudinal handling characteristics of a tailless gull-wing aircraft.” 2008. Web. 18 Jan 2021.

Vancouver:

Agenbag D. Longitudinal handling characteristics of a tailless gull-wing aircraft. [Internet] [Masters thesis]. University of Pretoria; 2008. [cited 2021 Jan 18]. Available from: http://hdl.handle.net/2263/28011.

Council of Science Editors:

Agenbag D. Longitudinal handling characteristics of a tailless gull-wing aircraft. [Masters Thesis]. University of Pretoria; 2008. Available from: http://hdl.handle.net/2263/28011

10. Mardanpour, Pezhman. Effects of engine placement and morphing on nonlinear aeroelastic behavior of flying wing aircraft.

Degree: PhD, Aerospace Engineering, 2013, Georgia Tech

 Effects of engine placement on flutter characteristics of a very flexible high-aspect-ratio wing are investigated using the code NATASHA (Nonlinear Aeroelastic Trim And Stability of… (more)

Subjects/Keywords: Nonlinear aeroelasticity; Follower force; Effects of engine placement; HALE aircraft; Flying wing aircraft; Area of minimum kinetic energy; Passive morphing; Solar powered flying wing; Airplanes, Tailless; Aeroelasticity; Solar airplanes; Airplanes

…INTRODUCTION 1.1 Flying wing aircraft A flying wing is a tailless fixed-wing aircraft with no… …73 98 Aircraft mass balance… …74 99 Effect of engine placement and aircraft center of gravity with zero offset from the… …75 100 Contour of normalized flutter speed at η = 0.65, keeping aircraft c.g. constant… …75 101 Contour of normalized flutter frequency at η = 0.65, keeping aircraft c.g. constant… 

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Mardanpour, P. (2013). Effects of engine placement and morphing on nonlinear aeroelastic behavior of flying wing aircraft. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/50268

Chicago Manual of Style (16th Edition):

Mardanpour, Pezhman. “Effects of engine placement and morphing on nonlinear aeroelastic behavior of flying wing aircraft.” 2013. Doctoral Dissertation, Georgia Tech. Accessed January 18, 2021. http://hdl.handle.net/1853/50268.

MLA Handbook (7th Edition):

Mardanpour, Pezhman. “Effects of engine placement and morphing on nonlinear aeroelastic behavior of flying wing aircraft.” 2013. Web. 18 Jan 2021.

Vancouver:

Mardanpour P. Effects of engine placement and morphing on nonlinear aeroelastic behavior of flying wing aircraft. [Internet] [Doctoral dissertation]. Georgia Tech; 2013. [cited 2021 Jan 18]. Available from: http://hdl.handle.net/1853/50268.

Council of Science Editors:

Mardanpour P. Effects of engine placement and morphing on nonlinear aeroelastic behavior of flying wing aircraft. [Doctoral Dissertation]. Georgia Tech; 2013. Available from: http://hdl.handle.net/1853/50268

.