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University: University of Manchester

You searched for subject:( wing camber ). Showing records 1 – 11 of 11 total matches.

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University of Manchester

1. Abdul Hamid, Mohd Faisal Bin. Aerodynamic models for insect flight.

Degree: 2016, University of Manchester

 Numerical models of insect flapping flight have previously been developed and used to simulate the performance of insect flight. These models were commonly developed via… (more)

Subjects/Keywords: flapping wing; insect flight; tandem wing

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APA (6th Edition):

Abdul Hamid, M. F. B. (2016). Aerodynamic models for insect flight. (Doctoral Dissertation). University of Manchester. Retrieved from http://www.manchester.ac.uk/escholar/uk-ac-man-scw:303191

Chicago Manual of Style (16th Edition):

Abdul Hamid, Mohd Faisal Bin. “Aerodynamic models for insect flight.” 2016. Doctoral Dissertation, University of Manchester. Accessed September 18, 2019. http://www.manchester.ac.uk/escholar/uk-ac-man-scw:303191.

MLA Handbook (7th Edition):

Abdul Hamid, Mohd Faisal Bin. “Aerodynamic models for insect flight.” 2016. Web. 18 Sep 2019.

Vancouver:

Abdul Hamid MFB. Aerodynamic models for insect flight. [Internet] [Doctoral dissertation]. University of Manchester; 2016. [cited 2019 Sep 18]. Available from: http://www.manchester.ac.uk/escholar/uk-ac-man-scw:303191.

Council of Science Editors:

Abdul Hamid MFB. Aerodynamic models for insect flight. [Doctoral Dissertation]. University of Manchester; 2016. Available from: http://www.manchester.ac.uk/escholar/uk-ac-man-scw:303191


University of Manchester

2. Abdul Hamid, Mohd Faisal. Aerodynamic models for insect flight.

Degree: PhD, 2016, University of Manchester

 Numerical models of insect flapping flight have previously been developed and used to simulate the performance of insect flight. These models were commonly developed via… (more)

Subjects/Keywords: 629.13; flapping wing; insect flight; tandem wing

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APA (6th Edition):

Abdul Hamid, M. F. (2016). Aerodynamic models for insect flight. (Doctoral Dissertation). University of Manchester. Retrieved from https://www.research.manchester.ac.uk/portal/en/theses/aerodynamic-models-for-insect-flight(057be27b-265a-45a0-b8d0-dc3c02a62a77).html ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.728093

Chicago Manual of Style (16th Edition):

Abdul Hamid, Mohd Faisal. “Aerodynamic models for insect flight.” 2016. Doctoral Dissertation, University of Manchester. Accessed September 18, 2019. https://www.research.manchester.ac.uk/portal/en/theses/aerodynamic-models-for-insect-flight(057be27b-265a-45a0-b8d0-dc3c02a62a77).html ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.728093.

MLA Handbook (7th Edition):

Abdul Hamid, Mohd Faisal. “Aerodynamic models for insect flight.” 2016. Web. 18 Sep 2019.

Vancouver:

Abdul Hamid MF. Aerodynamic models for insect flight. [Internet] [Doctoral dissertation]. University of Manchester; 2016. [cited 2019 Sep 18]. Available from: https://www.research.manchester.ac.uk/portal/en/theses/aerodynamic-models-for-insect-flight(057be27b-265a-45a0-b8d0-dc3c02a62a77).html ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.728093.

Council of Science Editors:

Abdul Hamid MF. Aerodynamic models for insect flight. [Doctoral Dissertation]. University of Manchester; 2016. Available from: https://www.research.manchester.ac.uk/portal/en/theses/aerodynamic-models-for-insect-flight(057be27b-265a-45a0-b8d0-dc3c02a62a77).html ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.728093


University of Manchester

3. El Ouardi, Othman. Design, Analysis And Testing Of An Aircraft Wing Model With Morphing Mechanism.

Degree: 2014, University of Manchester

Wing morphing has the potential to significantly improve the performance of an aircraft. The aerospace industry currently relies on control surfaces for changing aircraft wing(more)

Subjects/Keywords: Morphing wing; Adaptive wing; SMA; Variable thickness wing; Shape morphing; Smart materials

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APA (6th Edition):

El Ouardi, O. (2014). Design, Analysis And Testing Of An Aircraft Wing Model With Morphing Mechanism. (Doctoral Dissertation). University of Manchester. Retrieved from http://www.manchester.ac.uk/escholar/uk-ac-man-scw:237682

Chicago Manual of Style (16th Edition):

El Ouardi, Othman. “Design, Analysis And Testing Of An Aircraft Wing Model With Morphing Mechanism.” 2014. Doctoral Dissertation, University of Manchester. Accessed September 18, 2019. http://www.manchester.ac.uk/escholar/uk-ac-man-scw:237682.

MLA Handbook (7th Edition):

El Ouardi, Othman. “Design, Analysis And Testing Of An Aircraft Wing Model With Morphing Mechanism.” 2014. Web. 18 Sep 2019.

Vancouver:

El Ouardi O. Design, Analysis And Testing Of An Aircraft Wing Model With Morphing Mechanism. [Internet] [Doctoral dissertation]. University of Manchester; 2014. [cited 2019 Sep 18]. Available from: http://www.manchester.ac.uk/escholar/uk-ac-man-scw:237682.

Council of Science Editors:

El Ouardi O. Design, Analysis And Testing Of An Aircraft Wing Model With Morphing Mechanism. [Doctoral Dissertation]. University of Manchester; 2014. Available from: http://www.manchester.ac.uk/escholar/uk-ac-man-scw:237682


University of Manchester

4. Miller, Simon James. Adaptive wing structures for aeroelastic drag reduction and loads alleviation.

Degree: PhD, 2011, University of Manchester

 An investigation into two distinct novel adaptive structures concepts is performed with a view to improving the aerodynamic efficiency of aircraft wings.The main focus of… (more)

Subjects/Keywords: 629.13; Aeroelasticity; Aircraft morphing; Adaptive wing structures

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APA (6th Edition):

Miller, S. J. (2011). Adaptive wing structures for aeroelastic drag reduction and loads alleviation. (Doctoral Dissertation). University of Manchester. Retrieved from https://www.research.manchester.ac.uk/portal/en/theses/adaptive-wing-structures-for-aeroelastic-drag-reduction-and-loadsalleviation(562181ed-7153-44cb-b0c7-9bfe1f79ae0f).html ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.542701

Chicago Manual of Style (16th Edition):

Miller, Simon James. “Adaptive wing structures for aeroelastic drag reduction and loads alleviation.” 2011. Doctoral Dissertation, University of Manchester. Accessed September 18, 2019. https://www.research.manchester.ac.uk/portal/en/theses/adaptive-wing-structures-for-aeroelastic-drag-reduction-and-loadsalleviation(562181ed-7153-44cb-b0c7-9bfe1f79ae0f).html ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.542701.

MLA Handbook (7th Edition):

Miller, Simon James. “Adaptive wing structures for aeroelastic drag reduction and loads alleviation.” 2011. Web. 18 Sep 2019.

Vancouver:

Miller SJ. Adaptive wing structures for aeroelastic drag reduction and loads alleviation. [Internet] [Doctoral dissertation]. University of Manchester; 2011. [cited 2019 Sep 18]. Available from: https://www.research.manchester.ac.uk/portal/en/theses/adaptive-wing-structures-for-aeroelastic-drag-reduction-and-loadsalleviation(562181ed-7153-44cb-b0c7-9bfe1f79ae0f).html ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.542701.

Council of Science Editors:

Miller SJ. Adaptive wing structures for aeroelastic drag reduction and loads alleviation. [Doctoral Dissertation]. University of Manchester; 2011. Available from: https://www.research.manchester.ac.uk/portal/en/theses/adaptive-wing-structures-for-aeroelastic-drag-reduction-and-loadsalleviation(562181ed-7153-44cb-b0c7-9bfe1f79ae0f).html ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.542701


University of Manchester

5. Miller, Simon James. Adaptive wing structures for aeroelastic drag reduction and loadsalleviation.

Degree: 2011, University of Manchester

 An investigation into two distinct novel adaptive structures concepts is performed with a view to improving the aerodynamic efficiency of aircraft wings.The main focus of… (more)

Subjects/Keywords: Aeroelasticity; Aircraft morphing; Adaptive wing structures

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

APA (6th Edition):

Miller, S. J. (2011). Adaptive wing structures for aeroelastic drag reduction and loadsalleviation. (Doctoral Dissertation). University of Manchester. Retrieved from http://www.manchester.ac.uk/escholar/uk-ac-man-scw:120148

Chicago Manual of Style (16th Edition):

Miller, Simon James. “Adaptive wing structures for aeroelastic drag reduction and loadsalleviation.” 2011. Doctoral Dissertation, University of Manchester. Accessed September 18, 2019. http://www.manchester.ac.uk/escholar/uk-ac-man-scw:120148.

MLA Handbook (7th Edition):

Miller, Simon James. “Adaptive wing structures for aeroelastic drag reduction and loadsalleviation.” 2011. Web. 18 Sep 2019.

Vancouver:

Miller SJ. Adaptive wing structures for aeroelastic drag reduction and loadsalleviation. [Internet] [Doctoral dissertation]. University of Manchester; 2011. [cited 2019 Sep 18]. Available from: http://www.manchester.ac.uk/escholar/uk-ac-man-scw:120148.

Council of Science Editors:

Miller SJ. Adaptive wing structures for aeroelastic drag reduction and loadsalleviation. [Doctoral Dissertation]. University of Manchester; 2011. Available from: http://www.manchester.ac.uk/escholar/uk-ac-man-scw:120148


University of Manchester

6. Chard, James. Tangential leading edge blowing for flow control on non-slender delta wings.

Degree: 2018, University of Manchester

 In the military arena there is an increase in demand for Low Observable (LO) flight vehicles. This drive for low observability imposes limits on Leading… (more)

Subjects/Keywords: Leading edge blowing; Swept wing; Flow control; Fluidic control; Tangential blowing; Leading edge separation; Delta wing; UCAV

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APA (6th Edition):

Chard, J. (2018). Tangential leading edge blowing for flow control on non-slender delta wings. (Doctoral Dissertation). University of Manchester. Retrieved from http://www.manchester.ac.uk/escholar/uk-ac-man-scw:314613

Chicago Manual of Style (16th Edition):

Chard, James. “Tangential leading edge blowing for flow control on non-slender delta wings.” 2018. Doctoral Dissertation, University of Manchester. Accessed September 18, 2019. http://www.manchester.ac.uk/escholar/uk-ac-man-scw:314613.

MLA Handbook (7th Edition):

Chard, James. “Tangential leading edge blowing for flow control on non-slender delta wings.” 2018. Web. 18 Sep 2019.

Vancouver:

Chard J. Tangential leading edge blowing for flow control on non-slender delta wings. [Internet] [Doctoral dissertation]. University of Manchester; 2018. [cited 2019 Sep 18]. Available from: http://www.manchester.ac.uk/escholar/uk-ac-man-scw:314613.

Council of Science Editors:

Chard J. Tangential leading edge blowing for flow control on non-slender delta wings. [Doctoral Dissertation]. University of Manchester; 2018. Available from: http://www.manchester.ac.uk/escholar/uk-ac-man-scw:314613


University of Manchester

7. Chard, James. Tangential leading edge blowing for flow control on non-slender delta wings.

Degree: PhD, 2018, University of Manchester

 In the military arena there is an increase in demand for Low Observable (LO) flight vehicles. This drive for low observability imposes limits on Leading… (more)

Subjects/Keywords: Leading edge separation; Delta wing; UCAV; Tangential blowing; Swept wing; Flow control; Leading edge blowing; Fluidic control

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APA (6th Edition):

Chard, J. (2018). Tangential leading edge blowing for flow control on non-slender delta wings. (Doctoral Dissertation). University of Manchester. Retrieved from https://www.research.manchester.ac.uk/portal/en/theses/tangential-leading-edge-blowing-for-flow-control-on-nonslender-delta-wings(0ed0f6fa-23ad-44a2-a187-e8e1e8f1ac8a).html ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.748051

Chicago Manual of Style (16th Edition):

Chard, James. “Tangential leading edge blowing for flow control on non-slender delta wings.” 2018. Doctoral Dissertation, University of Manchester. Accessed September 18, 2019. https://www.research.manchester.ac.uk/portal/en/theses/tangential-leading-edge-blowing-for-flow-control-on-nonslender-delta-wings(0ed0f6fa-23ad-44a2-a187-e8e1e8f1ac8a).html ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.748051.

MLA Handbook (7th Edition):

Chard, James. “Tangential leading edge blowing for flow control on non-slender delta wings.” 2018. Web. 18 Sep 2019.

Vancouver:

Chard J. Tangential leading edge blowing for flow control on non-slender delta wings. [Internet] [Doctoral dissertation]. University of Manchester; 2018. [cited 2019 Sep 18]. Available from: https://www.research.manchester.ac.uk/portal/en/theses/tangential-leading-edge-blowing-for-flow-control-on-nonslender-delta-wings(0ed0f6fa-23ad-44a2-a187-e8e1e8f1ac8a).html ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.748051.

Council of Science Editors:

Chard J. Tangential leading edge blowing for flow control on non-slender delta wings. [Doctoral Dissertation]. University of Manchester; 2018. Available from: https://www.research.manchester.ac.uk/portal/en/theses/tangential-leading-edge-blowing-for-flow-control-on-nonslender-delta-wings(0ed0f6fa-23ad-44a2-a187-e8e1e8f1ac8a).html ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.748051


University of Manchester

8. Livshin, Rosalyn Diane. Nonconformity in the Manchester Jewish Community: The Case of Political Radicalism, 1889-1939.

Degree: 2015, University of Manchester

 The Jewish community in Britain has been characterised by its high degree of conformity. This study seeks to extend the parameters of Jewish life by… (more)

Subjects/Keywords: Jewish, Manchester, Nonconformity, Conformity, Radical Socialism,; Anarchism, Communism, Left-Wing

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

APA (6th Edition):

Livshin, R. D. (2015). Nonconformity in the Manchester Jewish Community: The Case of Political Radicalism, 1889-1939. (Doctoral Dissertation). University of Manchester. Retrieved from http://www.manchester.ac.uk/escholar/uk-ac-man-scw:262975

Chicago Manual of Style (16th Edition):

Livshin, Rosalyn Diane. “Nonconformity in the Manchester Jewish Community: The Case of Political Radicalism, 1889-1939.” 2015. Doctoral Dissertation, University of Manchester. Accessed September 18, 2019. http://www.manchester.ac.uk/escholar/uk-ac-man-scw:262975.

MLA Handbook (7th Edition):

Livshin, Rosalyn Diane. “Nonconformity in the Manchester Jewish Community: The Case of Political Radicalism, 1889-1939.” 2015. Web. 18 Sep 2019.

Vancouver:

Livshin RD. Nonconformity in the Manchester Jewish Community: The Case of Political Radicalism, 1889-1939. [Internet] [Doctoral dissertation]. University of Manchester; 2015. [cited 2019 Sep 18]. Available from: http://www.manchester.ac.uk/escholar/uk-ac-man-scw:262975.

Council of Science Editors:

Livshin RD. Nonconformity in the Manchester Jewish Community: The Case of Political Radicalism, 1889-1939. [Doctoral Dissertation]. University of Manchester; 2015. Available from: http://www.manchester.ac.uk/escholar/uk-ac-man-scw:262975

9. Ahmed Nabawy, Mostafa Ramadan. Design of Insect-Scale Flapping Wing Vehicles.

Degree: 2015, University of Manchester

 This thesis contributes to the state of the art in integrated design of insect-scale piezoelectric actuated flapping wing vehicles through the development of novel theoretical… (more)

Subjects/Keywords: flapping wing; aerodynamics; micro air vehicles; nano air vehicles; insect flight; rotary wing; induced power factor; figure of merit; leading-edge vortex; lifting line theory; optimum wing; optimum kinematics; piezoelectric actuators; dynamics; electromechanical coupling; unimorph; triple layer actuator; design; sizing

…Design of Insect-Scale Flapping Wing Vehicles 9.4 Results 244 9.5 Chapter Conclusions… …demonstrators of insect-like flapping wing air vehicles along with their biological counterparts. From… …56 9 Design of Insect-Scale Flapping Wing Vehicles Figure 2.6 (a) The flight… …57 Figure 2.7 Other rotary wing MAV designs. (a) Konkuk University design; image… …58 Figure 2.8 Cranfield University flapping wing rotor actuated with a piezoelectric… 

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

APA (6th Edition):

Ahmed Nabawy, M. R. (2015). Design of Insect-Scale Flapping Wing Vehicles. (Doctoral Dissertation). University of Manchester. Retrieved from http://www.manchester.ac.uk/escholar/uk-ac-man-scw:261284

Chicago Manual of Style (16th Edition):

Ahmed Nabawy, Mostafa Ramadan. “Design of Insect-Scale Flapping Wing Vehicles.” 2015. Doctoral Dissertation, University of Manchester. Accessed September 18, 2019. http://www.manchester.ac.uk/escholar/uk-ac-man-scw:261284.

MLA Handbook (7th Edition):

Ahmed Nabawy, Mostafa Ramadan. “Design of Insect-Scale Flapping Wing Vehicles.” 2015. Web. 18 Sep 2019.

Vancouver:

Ahmed Nabawy MR. Design of Insect-Scale Flapping Wing Vehicles. [Internet] [Doctoral dissertation]. University of Manchester; 2015. [cited 2019 Sep 18]. Available from: http://www.manchester.ac.uk/escholar/uk-ac-man-scw:261284.

Council of Science Editors:

Ahmed Nabawy MR. Design of Insect-Scale Flapping Wing Vehicles. [Doctoral Dissertation]. University of Manchester; 2015. Available from: http://www.manchester.ac.uk/escholar/uk-ac-man-scw:261284

10. Livshin, Rosalyn Diane. Nonconformity in the Manchester Jewish community : the case of political radicalism, 1889-1939.

Degree: PhD, 2015, University of Manchester

 The Jewish community in Britain has been characterised by its high degree of conformity. This study seeks to extend the parameters of Jewish life by… (more)

Subjects/Keywords: 320.53; Jewish; Manchester; Nonconformity; Conformity; Radical Socialism;

…the formation of a subculture of Marxist and secular left-wing Jews, who are still seen as… 

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

APA (6th Edition):

Livshin, R. D. (2015). Nonconformity in the Manchester Jewish community : the case of political radicalism, 1889-1939. (Doctoral Dissertation). University of Manchester. Retrieved from https://www.research.manchester.ac.uk/portal/en/theses/nonconformity-in-the-manchester-jewish-community-the-case-of-political-radicalism-18891939(f17ba44d-1495-4a85-8c14-de4cea39baa4).html ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.686743

Chicago Manual of Style (16th Edition):

Livshin, Rosalyn Diane. “Nonconformity in the Manchester Jewish community : the case of political radicalism, 1889-1939.” 2015. Doctoral Dissertation, University of Manchester. Accessed September 18, 2019. https://www.research.manchester.ac.uk/portal/en/theses/nonconformity-in-the-manchester-jewish-community-the-case-of-political-radicalism-18891939(f17ba44d-1495-4a85-8c14-de4cea39baa4).html ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.686743.

MLA Handbook (7th Edition):

Livshin, Rosalyn Diane. “Nonconformity in the Manchester Jewish community : the case of political radicalism, 1889-1939.” 2015. Web. 18 Sep 2019.

Vancouver:

Livshin RD. Nonconformity in the Manchester Jewish community : the case of political radicalism, 1889-1939. [Internet] [Doctoral dissertation]. University of Manchester; 2015. [cited 2019 Sep 18]. Available from: https://www.research.manchester.ac.uk/portal/en/theses/nonconformity-in-the-manchester-jewish-community-the-case-of-political-radicalism-18891939(f17ba44d-1495-4a85-8c14-de4cea39baa4).html ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.686743.

Council of Science Editors:

Livshin RD. Nonconformity in the Manchester Jewish community : the case of political radicalism, 1889-1939. [Doctoral Dissertation]. University of Manchester; 2015. Available from: https://www.research.manchester.ac.uk/portal/en/theses/nonconformity-in-the-manchester-jewish-community-the-case-of-political-radicalism-18891939(f17ba44d-1495-4a85-8c14-de4cea39baa4).html ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.686743

11. Nabawy, Mostafa. Design of insect-scale flapping wing vehicles.

Degree: PhD, 2015, University of Manchester

 This thesis contributes to the state of the art in integrated design of insect-scale piezoelectric actuated flapping wing vehicles through the development of novel theoretical… (more)

Subjects/Keywords: 629.132; flapping wing; aerodynamics; micro air vehicles; nano air vehicles; insect flight; rotary wing; induced power factor; figure of merit; leading-edge vortex; lifting line theory; optimum wing; optimum kinematics; piezoelectric actuators; dynamics; electromechanical coupling; unimorph; triple layer actuator; design; sizing

…Design of Insect-Scale Flapping Wing Vehicles 9.4 Results 244 9.5 Chapter Conclusions… …demonstrators of insect-like flapping wing air vehicles along with their biological counterparts. From… …56 9 Design of Insect-Scale Flapping Wing Vehicles Figure 2.6 (a) The flight… …57 Figure 2.7 Other rotary wing MAV designs. (a) Konkuk University design; image… …58 Figure 2.8 Cranfield University flapping wing rotor actuated with a piezoelectric… 

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

APA (6th Edition):

Nabawy, M. (2015). Design of insect-scale flapping wing vehicles. (Doctoral Dissertation). University of Manchester. Retrieved from https://www.research.manchester.ac.uk/portal/en/theses/design-of-insectscale-flapping-wing-vehicles(5720b8af-a755-4c54-beb6-ba6ef1a13168).html ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.644511

Chicago Manual of Style (16th Edition):

Nabawy, Mostafa. “Design of insect-scale flapping wing vehicles.” 2015. Doctoral Dissertation, University of Manchester. Accessed September 18, 2019. https://www.research.manchester.ac.uk/portal/en/theses/design-of-insectscale-flapping-wing-vehicles(5720b8af-a755-4c54-beb6-ba6ef1a13168).html ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.644511.

MLA Handbook (7th Edition):

Nabawy, Mostafa. “Design of insect-scale flapping wing vehicles.” 2015. Web. 18 Sep 2019.

Vancouver:

Nabawy M. Design of insect-scale flapping wing vehicles. [Internet] [Doctoral dissertation]. University of Manchester; 2015. [cited 2019 Sep 18]. Available from: https://www.research.manchester.ac.uk/portal/en/theses/design-of-insectscale-flapping-wing-vehicles(5720b8af-a755-4c54-beb6-ba6ef1a13168).html ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.644511.

Council of Science Editors:

Nabawy M. Design of insect-scale flapping wing vehicles. [Doctoral Dissertation]. University of Manchester; 2015. Available from: https://www.research.manchester.ac.uk/portal/en/theses/design-of-insectscale-flapping-wing-vehicles(5720b8af-a755-4c54-beb6-ba6ef1a13168).html ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.644511

.