See the published version of this preprint at Advances in Aerodynamics.
This is a preprint, a preliminary version of a manuscript that has not completed peer review at a journal. Research Square does not conduct peer review prior to posting preprints. The posting of a preprint on this server should not be interpreted as an endorsement of its validity or suitability for dissemination as established information or for guiding clinical practice.
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Research
Yongwei Gao
Northwestern Polytechnical University
Corresponding Author
ORCiD: https://orcid.org/0000-0001-7026-9273
License:
This work is licensed under a CC BY 4.0 License. Read Full License
The effectiveness of the Vectored Thrust Ducted Propeller (VTDP) system is not high currently, especially the lateral force is not large enough. Thus, a conceptual design for a deflection device of a VTDP system was proposed to achieve effective hovering control. The magnitude of the lateral force that was applied to maintain balance while hovering was examined. A comparison between the experimental and numerical results for the 16H-1 was made to verify the numerical simulation approach. The deflection devices of the X-49 and the proposed design were analyzed using numerical simulations. The results indicated that a larger lateral force and lower power consumption were presented in the proposed design. The results of this article provide a new idea for the design of the VTDP system.
Keywords
vectored thrust ducted propeller, conceptual design, wind tunnel experiment, numerical simulation
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CURRENT STATUS: Published
View the published article at Advances in Aerodynamics.
Version 2
Posted 15 Oct, 2020
Community comments: 1
Review #1 received
Received 13 Oct, 2020
Editorial decision: Accept
On 13 Oct, 2020
Reviewers invited
Invitations sent on 08 Oct, 2020
Reviewer #1 agreed
On 08 Oct, 2020
Editor assigned
On 06 Oct, 2020
Submission checks complete
On 05 Oct, 2020
Editor invited
On 05 Oct, 2020
No comments provided
Editorial decision: Major revision
On 16 Sep, 2020
Review #2 received
Received 15 Sep, 2020
Reviewer #2 agreed
On 05 Sep, 2020
Review #1 received
Received 02 Sep, 2020
Reviewer #1 agreed
On 29 Aug, 2020
Reviewers invited
Invitations sent on 25 Aug, 2020
First submitted
On 24 Aug, 2020
Editor assigned
On 24 Aug, 2020
Submission checks complete
On 23 Aug, 2020
Editor invited
On 23 Aug, 2020
Metrics
Comments: 0
PDF Downloads: ...
HTML Views: ...
Subject Areas
Aeronautics and Astronautics
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See the published version of this preprint at Advances in Aerodynamics.
This is a preprint, a preliminary version of a manuscript that has not completed peer review at a journal. Research Square does not conduct peer review prior to posting preprints. The posting of a preprint on this server should not be interpreted as an endorsement of its validity or suitability for dissemination as established information or for guiding clinical practice.
Learn more about In Review
Research
Yongwei Gao
Northwestern Polytechnical University
Corresponding Author
ORCiD: https://orcid.org/0000-0001-7026-9273
Badges
Prescreen
This manuscript passed our Prescreen assessment
Complete author information
Appropriate declaration statements
Potential risks to human health
Prescreen
Peer Review Timeline
CURRENT STATUS: Published
View the published article at Advances in Aerodynamics.
Version 2
Posted 15 Oct, 2020
Community comments: 1
Review #1 received
Received 13 Oct, 2020
Editorial decision: Accept
On 13 Oct, 2020
Reviewers invited
Invitations sent on 08 Oct, 2020
Reviewer #1 agreed
On 08 Oct, 2020
Editor assigned
On 06 Oct, 2020
Submission checks complete
On 05 Oct, 2020
Editor invited
On 05 Oct, 2020
No comments provided
Editorial decision: Major revision
On 16 Sep, 2020
Review #2 received
Received 15 Sep, 2020
Reviewer #2 agreed
On 05 Sep, 2020
Review #1 received
Received 02 Sep, 2020
Reviewer #1 agreed
On 29 Aug, 2020
Reviewers invited
Invitations sent on 25 Aug, 2020
First submitted
On 24 Aug, 2020
Editor assigned
On 24 Aug, 2020
Submission checks complete
On 23 Aug, 2020
Editor invited
On 23 Aug, 2020
Metrics
Comments: 0
PDF Downloads: ...
HTML Views: ...
Subject Areas
Aeronautics and Astronautics
License:
This work is licensed under a CC BY 4.0 License. Read Full License
View the published article at Advances in Aerodynamics.
The effectiveness of the Vectored Thrust Ducted Propeller (VTDP) system is not high currently, especially the lateral force is not large enough. Thus, a conceptual design for a deflection device of a VTDP system was proposed to achieve effective hovering control. The magnitude of the lateral force that was applied to maintain balance while hovering was examined. A comparison between the experimental and numerical results for the 16H-1 was made to verify the numerical simulation approach. The deflection devices of the X-49 and the proposed design were analyzed using numerical simulations. The results indicated that a larger lateral force and lower power consumption were presented in the proposed design. The results of this article provide a new idea for the design of the VTDP system.
Figure 1
Figure 2
Figure 3
Figure 4
Figure 5
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Figure 9
Figure 10
Figure 11
Figure 12
Figure 13
Figure 14
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Figure 27
Figure 28
Figure 29
Figure 30
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