Example of International Journal of Engineering Systems Modelling and Simulation format
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Example of International Journal of Engineering Systems Modelling and Simulation format Example of International Journal of Engineering Systems Modelling and Simulation format Example of International Journal of Engineering Systems Modelling and Simulation format Example of International Journal of Engineering Systems Modelling and Simulation format
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Example of International Journal of Engineering Systems Modelling and Simulation format Example of International Journal of Engineering Systems Modelling and Simulation format Example of International Journal of Engineering Systems Modelling and Simulation format Example of International Journal of Engineering Systems Modelling and Simulation format
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This content is only for preview purposes. The original open access content can be found here.
open access Open Access

International Journal of Engineering Systems Modelling and Simulation — Template for authors

Categories Rank Trend in last 3 yrs
Engineering (all) #167 of 297 up up by 20 ranks
Modeling and Simulation #224 of 290 up up by 1 rank
journal-quality-icon Journal quality:
Medium
calendar-icon Last 4 years overview: 72 Published Papers | 90 Citations
indexed-in-icon Indexed in: Scopus
last-updated-icon Last updated: 23/06/2020
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Related Journals

open access Open Access

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Quality:  
High
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SJR: 1.624
SNIP: 1.688
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SJR: 0.264
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Quality:  
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CiteRatio: 8.9
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Journal Performance & Insights

CiteRatio

SCImago Journal Rank (SJR)

Source Normalized Impact per Paper (SNIP)

A measure of average citations received per peer-reviewed paper published in the journal.

Measures weighted citations received by the journal. Citation weighting depends on the categories and prestige of the citing journal.

Measures actual citations received relative to citations expected for the journal's category.

1.3

18% from 2019

CiteRatio for International Journal of Engineering Systems Modelling and Simulation from 2016 - 2020
Year Value
2020 1.3
2019 1.1
2018 0.7
2017 0.6
2016 0.6
graph view Graph view
table view Table view

0.16

6% from 2019

SJR for International Journal of Engineering Systems Modelling and Simulation from 2016 - 2020
Year Value
2020 0.16
2019 0.171
2018 0.128
2017 0.175
2016 0.161
graph view Graph view
table view Table view

0.241

48% from 2019

SNIP for International Journal of Engineering Systems Modelling and Simulation from 2016 - 2020
Year Value
2020 0.241
2019 0.463
2018 0.245
2017 0.422
2016 0.306
graph view Graph view
table view Table view

insights Insights

  • CiteRatio of this journal has increased by 18% in last years.
  • This journal’s CiteRatio is in the top 10 percentile category.

insights Insights

  • SJR of this journal has decreased by 6% in last years.
  • This journal’s SJR is in the top 10 percentile category.

insights Insights

  • SNIP of this journal has decreased by 48% in last years.
  • This journal’s SNIP is in the top 10 percentile category.

International Journal of Engineering Systems Modelling and Simulation

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Inderscience Publishers

International Journal of Engineering Systems Modelling and Simulation

Approved by publishing and review experts on SciSpace, this template is built as per for International Journal of Engineering Systems Modelling and Simulation formatting guidelines as mentioned in Inderscience Publishers author instructions. The current version was created on 23 Jun 2020 and has been used by 999 authors to write and format their manuscripts to this journal.

i
Last updated on
23 Jun 2020
i
ISSN
1755-9758
i
Impact Factor
Low - 0.482
i
Open Access
No
i
Sherpa RoMEO Archiving Policy
Yellow faq
i
Plagiarism Check
Available via Turnitin
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Endnote Style
Download Available
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Bibliography Name
plainnat
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Citation Type
Author Year
(Blonder et al., 1982)
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Bibliography Example
Beenakker, C. W. J. (2006). ‘Specular Andreev Reflection in Graphene’. Phys. Rev. Lett., Vol 97, No 6, pp. 067007.

Top papers written in this journal

Journal Article DOI: 10.1504/IJESMS.2010.031877
Roughness receptivity in swept-wing boundary layers – experiments
Andrew L. Carpenter1, William S. Saric1, Helen L. Reed1

Abstract:

The receptivity of boundary layer stability to micron-sized, spanwise-periodic discrete roughness elements (DREs) was studied. The DREs were applied to the leading edge of a 30-degree swept-wing. The test article was attached vertically to the port wing of a Cessna O-2A aircraft and operated at a chord Reynolds number of 6.5 ... The receptivity of boundary layer stability to micron-sized, spanwise-periodic discrete roughness elements (DREs) was studied. The DREs were applied to the leading edge of a 30-degree swept-wing. The test article was attached vertically to the port wing of a Cessna O-2A aircraft and operated at a chord Reynolds number of 6.5 to 7.5 million. Critically spaced DREs were applied at the leading edge to excite the crossflow instability and move transition forward. In this case, calibrated, multi-element hotfilm sensors were used to measure disturbance wall shear stress. The roughness height was varied from 0 to 50 microns both in the positive (bumps) and negative (dimples) sense. Thus, the disturbance amplitude variations were determined as a function of modulated DRE heights. read more read less

Topics:

Leading edge (57%)57% related to the paper, Boundary layer (53%)53% related to the paper, Swept wing (53%)53% related to the paper, Chord (aeronautics) (52%)52% related to the paper
39 Citations
Journal Article DOI: 10.1504/IJESMS.2013.052386
Boundary-layer instability and transition on a flared cone in a Mach 6 quiet wind tunnel
Jerrod W. Hofferth1, William S. Saric1, Joseph Kuehl1, Eduardo Pérez1, Travis S. Kocian1, Helen L. Reed1

Abstract:

Measurements of boundary-layer transition location and boundary layer profiles on a sharp-tipped 5o-half-angle flared cone were made in a low-disturbance Mach 6 wind tunnel. Uncalibrated boundary-layer profiles of mean and fluctuating voltage representative of mass flux are obtained using constant temperature hot-wire anemome... Measurements of boundary-layer transition location and boundary layer profiles on a sharp-tipped 5o-half-angle flared cone were made in a low-disturbance Mach 6 wind tunnel. Uncalibrated boundary-layer profiles of mean and fluctuating voltage representative of mass flux are obtained using constant temperature hot-wire anemometry at several axial locations, and are notionally compared with preliminary simulations. Spectral energy content is observed between 250 and 310 kHz – the first measurements of frequencies typical of the second mode instability at Texas A&M. Growth of this high-frequency content is compared with N-factor results from linear parabolised stability equation (LPSE) computations. Possible sources of disagreement between the experimental and computed frequencies for second-mode growth are discussed, as are future improvements to the hotwire anemometry technique. Nevertheless, the successful measurement of high-frequency content highlighted here constitutes an important step toward acquisition of calibrated measurements of hypersonic boundary-layer instabilities to be used as code validation. read more read less

Topics:

Wind tunnel (55%)55% related to the paper, Mach number (55%)55% related to the paper, Hypersonic speed (54%)54% related to the paper, Aerodynamics (53%)53% related to the paper, Boundary layer (53%)53% related to the paper
39 Citations
open accessOpen access Journal Article DOI: 10.1504/IJESMS.2008.018845
Diesel fuel spray penetration, heating, evaporation and ignition: modelling vs. experimentation
Sergei Sazhin1, Sergey Martynov2, T. Kristyadi, Cyril Crua1, Morgan Heikal1

Abstract:

The modified WAVE droplet breakup model, taking into account the transient processes during spray injection, the Effective Thermal Conductivity (ETC) liquid phase model, the gas phase model suggested by Abramzon and Sirignano, and the customised version of the Shell autoignition model have been implemented into the KIVA 2 CFD... The modified WAVE droplet breakup model, taking into account the transient processes during spray injection, the Effective Thermal Conductivity (ETC) liquid phase model, the gas phase model suggested by Abramzon and Sirignano, and the customised version of the Shell autoignition model have been implemented into the KIVA 2 CFD code. The observed Diesel spray tip penetration and Sauter Mean Radii show much better agreement with the prediction of the modified WAVE model compared with other droplet breakup models. The difference in the autoignition delay times predicted using the Infinite Thermal Conductivity (ITC) and ETC models is important for practical computations. read more read less

Topics:

Autoignition temperature (55%)55% related to the paper
View PDF
35 Citations
Journal Article DOI: 10.1504/IJESMS.2009.027576
Modelling, validation and roll moment rejection control of pneumatically actuated active roll control for improving vehicle lateral dynamics performance
Khisbullah Hudha1, Zulkiffli Abd Kadir1, Md. Radzai Said1, Hishamuddin Jamaluddin2

Abstract:

This paper presents a detailed derivation of a full vehicle model and validation using an instrumented experimental vehicle. Two types of vehicle dynamics test are performed for the purpose of model validation namely step steer test and double lane change test. The results of model validation show that the behaviours of the m... This paper presents a detailed derivation of a full vehicle model and validation using an instrumented experimental vehicle. Two types of vehicle dynamics test are performed for the purpose of model validation namely step steer test and double lane change test. The results of model validation show that the behaviours of the model closely follow the behaviour of a real vehicle. An active roll control (ARC) suspension system is then developed on the validated full vehicle model to reduce unwanted vehicle motions during cornering manoeuvres. The proposed controller structure for the ARC system is PID control with roll moment rejection loop. The results of the study show that the proposed control structure is able to significantly improve the dynamics performance of the vehicle compared to the passive vehicle system. The additional roll moment rejection loop is able to further improve the performance of the PID controller for the ARC system. read more read less

Topics:

Roll moment (68%)68% related to the paper, Vehicle dynamics (59%)59% related to the paper, Control theory (53%)53% related to the paper, PID controller (53%)53% related to the paper
30 Citations
Journal Article DOI: 10.1504/IJESMS.2010.031874
Assessment of intrusive and non-intrusive non-deterministic CFD methodologies based on polynomial chaos expansions

Abstract:

The paper presents the computational results of an ongoing validation effort of two polynomial chaos methods used in the non-deterministic simulations of the transonic flow in the NASA Rotor 37 axial compressor. In the first stage, a code to code comparison on the geometry of the NASA Rotor 37 allows exploring different influ... The paper presents the computational results of an ongoing validation effort of two polynomial chaos methods used in the non-deterministic simulations of the transonic flow in the NASA Rotor 37 axial compressor. In the first stage, a code to code comparison on the geometry of the NASA Rotor 37 allows exploring different influences on the computed mean and standard deviation of the pressure field and output functionals of interest as the inlet mass flow rate, the isentropic efficiency and the pressure ratio. The validation results are concerned with the management of two uncertainties: one of operational origin imposed on the outlet static pressure boundary condition and another one of geometrical nature the tip clearance particularly. These results are displayed as non-deterministic compressor maps and graphs showing the dependency of the functionals' coefficients of variations with respect to the inlet mass flow rate. Finally, our conclusions on the employed computational programme are drawn. read more read less

Topics:

Polynomial chaos (56%)56% related to the paper, Gas compressor (54%)54% related to the paper, Axial compressor (54%)54% related to the paper, Computational fluid dynamics (52%)52% related to the paper, Static pressure (51%)51% related to the paper
27 Citations
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Frequently asked questions

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13. What is Sherpa RoMEO Archiving Policy for International Journal of Engineering Systems Modelling and Simulation?

SHERPA/RoMEO Database

We extracted this data from Sherpa Romeo to help researchers understand the access level of this journal in accordance with the Sherpa Romeo Archiving Policy for International Journal of Engineering Systems Modelling and Simulation. The table below indicates the level of access a journal has as per Sherpa Romeo's archiving policy.

RoMEO Colour Archiving policy
Green Can archive pre-print and post-print or publisher's version/PDF
Blue Can archive post-print (ie final draft post-refereeing) or publisher's version/PDF
Yellow Can archive pre-print (ie pre-refereeing)
White Archiving not formally supported
FYI:
  1. Pre-prints as being the version of the paper before peer review and
  2. Post-prints as being the version of the paper after peer-review, with revisions having been made.

14. What are the most common citation types In International Journal of Engineering Systems Modelling and Simulation?

The 5 most common citation types in order of usage for International Journal of Engineering Systems Modelling and Simulation are:.

S. No. Citation Style Type
1. Author Year
2. Numbered
3. Numbered (Superscripted)
4. Author Year (Cited Pages)
5. Footnote

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