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Article
Peer-Review Record

Robust Optimization Design of the Aerodynamic Shape and External Ballistics of a Pulse Trajectory Correction Projectile

Appl. Sci. 2023, 13(12), 7007; https://doi.org/10.3390/app13127007
by Bingnan Xing 1, Chengxin Du 1, Zhonghua Du 1,* and Wenxin Yang 2
Reviewer 1: Anonymous
Reviewer 2:
Appl. Sci. 2023, 13(12), 7007; https://doi.org/10.3390/app13127007
Submission received: 14 May 2023 / Revised: 5 June 2023 / Accepted: 6 June 2023 / Published: 10 June 2023

Round 1

Reviewer 1 Report

This paper focuses on trajectory correction projectiles with lateral pulses as the research object. It takes into account the inherent uncertain factors in engineering calculations and carries out a robust optimization design for the aerodynamic shape and exterior ballistics. The research is attractive for several engineering applications. The paper is quite well organized, and it has a good quality, however some requests can further improve its quality.

In the introduction you should add more references on aerodynamic CFD methods applications; moreover you should enlarge the part on the UQ works with also other recent applications.

In particular I suggest for example these references:

-  Xia, L., Zou, Z. J., Wang, Z. H., Zou, L., & Gao, H. Surrogate model based uncertainty quantification of CFD simulations of the viscous flow around a ship advancing in shallow water. Ocean Engineering 2021, 234, 109206

- Cravero, C.; De Domenico, D.; Marsano, D. The Use of Uncertainty Quantification and Numerical Optimization to Support the Design and Operation Management of Air-Staging Gas Recirculation Strategies in Glass Furnaces. Fluids 2023, 8, 76.

- Cravero, C; De Domenico, D; Marsano, D. “Uncertainty Quantification Analysis of Exhaust Gas Plume in a Crosswind”. Energies, 2023, Vol. 16, Issue 8, p. 3549.

The optimization design process has been well described, as well as the rest of the theoretical foundation.

For the design problem you should ad more geometrical data also superimposed on a figure.

The mesh has been reported and a grid sensitivity analysis has been performed, however more details on the cells sizes must be provided (minimum, maximum, quality, prism layer?). Moreover the CFD model must be better described (models used, boundary condition, scheme order, etc..)

The results with also the validation are clear and accurate.

The conclusions well summarize the main target obtained.

Minor corrections

Author Response

Please see the attachment.

Author Response File: Author Response.docx

Reviewer 2 Report

This article is dedicated to a sound full subject but restricted to defense specialist. 

The paper is well written and describe a high quality research work.
Nevertheless I would like to ask for some corrections before publications :

     Citing 12 references in the same sentences without any real information about them is not the way to do (cf lines 31-32). Same remarks line 71. Speaking about references I think that ISL work especially from Gnemmi et al. and Nekris et al. should have been added to the references and even better discussed and compared to the present work.

I also would like to have more details about the CFD simulations : code used ? physical and numerical model used, mesh convergence study, y+, minimum space step size, cfl etc... 

Author Response

Please see the attachment.

Author Response File: Author Response.docx

Reviewer 3 Report

Please see the attached file.

Comments for author File: Comments.docx

Minor revisions are required.

Author Response

Please see the attachment.

Author Response File: Author Response.docx

Round 2

Reviewer 1 Report

All my requestes have been correctly addressed and added in the revsied work. Now its is ready for the publication in this form, by having increased its quality

Author Response

Thanks for your comments.

Reviewer 3 Report

Please see attached file.

Comments for author File: Comments.pdf

Author Response

Please see the response in the attached file.

Author Response File: Author Response.docx

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