Next Article in Journal
Morphology Control and Metallization of Porous Polymers Synthesized by Michael Addition Reactions of a Multi-Functional Acrylamide with a Diamine
Next Article in Special Issue
Sustainable End-of-Life Management of Wind Turbine Blades: Overview of Current and Coming Solutions
Previous Article in Journal
Single-Stroke Attachment of Sheets to Tube Ends Made from Dissimilar Materials
 
 
Article
Peer-Review Record

Aircraft Impact Effects on an Aged NPP

Materials 2021, 14(4), 816; https://doi.org/10.3390/ma14040816
by Rosa Lo Frano
Reviewer 1: Anonymous
Reviewer 2: Anonymous
Reviewer 3:
Materials 2021, 14(4), 816; https://doi.org/10.3390/ma14040816
Submission received: 3 December 2020 / Revised: 19 January 2021 / Accepted: 29 January 2021 / Published: 8 February 2021

Round 1

Reviewer 1 Report

The paper concerns the modeling of deformation processes that occur during the dynamic interaction of a flying missile and a reinforced concrete target.

The essence of mathematical modeling is presented very superficially, only the verbal formulation of the problem is given and the MARC package options used are mentioned. The absence of a mathematical formulation of the problem makes it difficult to understand the essence of the mathematical model of the considered physical processes.

In particular, it is impossible to understand from the text which version of the model of elastoplastic deformation is used. It is impossible to assess how the physical properties of construction materials change during aging. The text does not provide information on how the processes of fragmentation of colliding bodies are modeled.

This raises the question of how the mechanical properties of the projectile and design materials are taken into account. Table 1 lists only the properties of the metal components of the structure. It does not say anything about the properties of concrete and missile. In addition, the tabular data refer to low-speed deformation processes.The author does not substantiate the possibility of their use in modeling high-speed processes where the limiting characteristics depend on the deformation rate.

These circumstances do not allow us to assess the reliability of the results obtained, although the words concerning the nature of the deformation interaction do not raise objections. The words about the very good agreement between the results of simulation and full-scale aircraft impact test are only descriptive.

Notes on the article design

Line 75-76           7m2 wide             either the linear dimensions of the target, or its area

Fig 3b    figure caption is incomprehensible, there is no dimension for the scale

Fig 3, 4 what moment in time do the pictures correspond to?

Fig 9      the upper graph is unreadable, there is no explanation to this sraph

Fig 10 a, b, Fig 11             what moment in time do the pictures correspond to?; scales have no dimensions

Fig 12    no explanation of what lines 1, 2, 3 mean

Author Response

Please see the attachment

Author Response File: Author Response.pdf

Reviewer 2 Report

Some images have a low resolution (they are not quite clear)

 

 

Author Response

Please see the attachment

Author Response File: Author Response.pdf

Reviewer 3 Report

In the present manuscript, the study addressed the numerical simulation of an aged NPPs subjected to an aircraft impact. The effects of impact velocity, direction and location were investigated together with the unfavourable conditions to be expected for the plant. Firstly, the numerical model was validated based on the results obtained from the experiments of Sugano et al. Through the results comparation between the aged an unaged NPPs, the author showed that ageing increases the plant propensity to suffer extensive, even penetration. Meanwhile, the research indicated that the damage at the impact area confirmed to be dependent on the type of aircraft and target wall thickness has a great important meaning not only in the academic but also in the practical engineering. I recommend to accept it after major revisions, the following aspects should be paid attentions:

(1) In the abstract, line 12, the expression that “This study addresses the numerical simulation of an aged NPP subjected to a large commercial aircraft impact”. But in the manuscript only the F-4 fighter was used, which is not a large commercial aircraft.

(2) Line 166, author expressed the two-strike locations have been selected:1) just above the equipment hatch; 2) on the dome. However, the equipment hatch location was not found in FEM model. Then in the simulation discussion section, there were no relevant results or explanation.

(3) The manuscript does not describe the material behaviour of the concrete and the steel materials. The study is based on a highly nonlinear analysis and the deformations would be strain rate dependent. No explanation has been given regarding modelling the behaviour of material, either for steel or concrete. Table 1 is insufficient to describe the behaviour of concrete for the problem studied.

(4) The author should describe the difference between aged and unaged concrete of containment material behavior.

(5) The containment model mesh gird is relevant large (4.5 m element size estimated). In previous published papers(Zou & Sui et al. The Structural Design of Tall and Special Buildings, 2019, 28(16)), the mesh gird adopted should be fine enough. Please explain the reason and the reasonableness of the results based on the mesh size.

Author Response

Please see the attachment

Author Response File: Author Response.pdf

Round 2

Reviewer 3 Report

Accept

Back to TopTop