Example of International Journal of Aerospace Engineering format
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Example of International Journal of Aerospace Engineering format Example of International Journal of Aerospace Engineering format Example of International Journal of Aerospace Engineering format Example of International Journal of Aerospace Engineering format Example of International Journal of Aerospace Engineering format Example of International Journal of Aerospace Engineering format Example of International Journal of Aerospace Engineering format Example of International Journal of Aerospace Engineering format Example of International Journal of Aerospace Engineering format Example of International Journal of Aerospace Engineering format
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Example of International Journal of Aerospace Engineering format Example of International Journal of Aerospace Engineering format Example of International Journal of Aerospace Engineering format Example of International Journal of Aerospace Engineering format Example of International Journal of Aerospace Engineering format Example of International Journal of Aerospace Engineering format Example of International Journal of Aerospace Engineering format Example of International Journal of Aerospace Engineering format Example of International Journal of Aerospace Engineering format Example of International Journal of Aerospace Engineering format
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open access Open Access

International Journal of Aerospace Engineering — Template for authors

Publisher: Hindawi
Categories Rank Trend in last 3 yrs
Aerospace Engineering #67 of 129 down down by 7 ranks
journal-quality-icon Journal quality:
Medium
calendar-icon Last 4 years overview: 577 Published Papers | 1138 Citations
indexed-in-icon Indexed in: Scopus
last-updated-icon Last updated: 26/06/2020
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Related Journals

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Quality:  
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CiteRatio: 3.7
SJR: 0.396
SNIP: 1.133
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SJR: 1.137
SNIP: 2.134
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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.

2.0

11% from 2019

CiteRatio for International Journal of Aerospace Engineering from 2016 - 2020
Year Value
2020 2.0
2019 1.8
2018 1.6
2017 1.3
2016 1.0
graph view Graph view
table view Table view

0.361

6% from 2019

SJR for International Journal of Aerospace Engineering from 2016 - 2020
Year Value
2020 0.361
2019 0.342
2018 0.29
2017 0.232
2016 0.203
graph view Graph view
table view Table view

0.8

17% from 2019

SNIP for International Journal of Aerospace Engineering from 2016 - 2020
Year Value
2020 0.8
2019 0.967
2018 0.879
2017 0.842
2016 0.812
graph view Graph view
table view Table view

insights Insights

  • CiteRatio of this journal has increased by 11% in last years.
  • This journal’s CiteRatio is in the top 10 percentile category.

insights Insights

  • SJR of this journal has increased 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 17% in last years.
  • This journal’s SNIP is in the top 10 percentile category.
International Journal of Aerospace Engineering

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Hindawi

International Journal of Aerospace Engineering

International Journal of Aerospace Engineering aims to serve the international aerospace engineering community through dissemination of scientific knowledge on practical engineering and design methodologies pertaining to aircraft and space vehicles. Original unpublished manusc...... Read More

Engineering

i
Last updated on
25 Jun 2020
i
ISSN
1687-5966
i
Impact Factor
High - 1.151
i
Acceptance Rate
30%
i
Frequency
Not provided
i
Open Access
Yes
i
Sherpa RoMEO Archiving Policy
Green faq
i
Plagiarism Check
Available via Turnitin
i
Endnote Style
Download Available
i
Bibliography Name
unsrt
i
Citation Type
Numbered
[25]
i
Bibliography Example
C. W. J. Beenakker. “Specular andreev reflection in graphene”. Phys. Rev. Lett., vol. 97, no. 6, 067007, 2006.

Top papers written in this journal

open accessOpen access Journal Article DOI: 10.1155/2011/154798
Reengineering Aircraft Structural Life Prediction Using a Digital Twin

Abstract:

Reengineering of the aircraft structural life prediction process to fully exploit advances in very high performance digital computing is proposed. The proposed process utilizes an ultrahigh fidelity model of individual aircraft by tail number, a Digital Twin, to integrate computation of structural deflections and temperatures... Reengineering of the aircraft structural life prediction process to fully exploit advances in very high performance digital computing is proposed. The proposed process utilizes an ultrahigh fidelity model of individual aircraft by tail number, a Digital Twin, to integrate computation of structural deflections and temperatures in response to flight conditions, with resulting local damage and material state evolution. A conceptual model of how the Digital Twin can be used for predicting the life of aircraft structure and assuring its structural integrity is presented. The technical challenges to developing and deploying a Digital Twin are discussed in detail. read more read less
View PDF
681 Citations
open accessOpen access Journal Article DOI: 10.1155/2019/5063145
Towards the Thousandth CubeSat: A Statistical Overview
Thyrso Villela1, Cesar A. Costa, Alessandra Brandão, Fernando T. Bueno, Rodrigo Leonardi

Abstract:

CubeSats have become an interesting innovation in the space sector. Such platforms are being used for several space applications, such as education, Earth remote sensing, science, and defense. As of May 31st, 2018, 855 CubeSats had been launched. Remote sensing application is the main sector in which CubeSats are being used, ... CubeSats have become an interesting innovation in the space sector. Such platforms are being used for several space applications, such as education, Earth remote sensing, science, and defense. As of May 31st, 2018, 855 CubeSats had been launched. Remote sensing application is the main sector in which CubeSats are being used, corresponding to about 45% of all applications. This fact indicates the commercial potential of such a platform. Fifty eight countries have already been involved with developing CubeSats. The most used CubeSat configuration is 3U (about 64%), followed by 1U (18%), while 6U platforms account for about 4%. In this paper, we present an analysis of the current situation regarding CubeSats worldwide, through the use of a dataset built to encompass information about these satellites. The overall success rate of the CubeSat missions is increasing over time. Moreover, considering CubeSat missions as a Bernoulli experiment, and excluding launch failures, the current success rate was estimated, as a parameter of a binomial distribution, to be about 75%. By using a logistic model and considering that the launchings keep following the current tendency, one can expect that one thousand CubeSats will be launched in 2021, within 95% certainty. read more read less

Topics:

CubeSat (59%)59% related to the paper
View PDF
159 Citations
open accessOpen access Journal Article DOI: 10.1155/2012/121802
Recent Experimental Efforts on High-Pressure Supercritical Injection for Liquid Rockets and Their Implications

Abstract:

Pressure and temperature of the liquid rocket thrust chambers into which propellants are injected have been in an ascending trajectory to gain higher specific impulse. It is quite possible then that the thermodynamic condition into which liquid propellants are injected reaches or surpasses the critical point of one or more of... Pressure and temperature of the liquid rocket thrust chambers into which propellants are injected have been in an ascending trajectory to gain higher specific impulse. It is quite possible then that the thermodynamic condition into which liquid propellants are injected reaches or surpasses the critical point of one or more of the injected fluids. For example, in cryogenic hydrogen/oxygen liquid rocket engines, such as Space Shuttle Main Engine (SSME) or Vulcain (Ariane 5), the injected liquid oxygen finds itself in a supercritical condition. Very little detailed information was available on the behavior of liquid jets under such a harsh environment nearly two decades ago. The author had the opportunity to be intimately involved in the evolutionary understanding of injection processes at the Air Force Research Laboratory (AFRL), spanning sub- to supercritical conditions during this period. The information included here attempts to present a coherent summary of experimental achievements pertinent to liquid rockets, focusing only on the injection of nonreacting cryogenic liquids into a high-pressure environment surpassing the critical point of at least one of the propellants. Moreover, some implications of the results acquired under such an environment are offered in the context of the liquid rocket combustion instability problem. read more read less

Topics:

Liquid-propellant rocket (64%)64% related to the paper, Liquid oxygen (60%)60% related to the paper, Rocket propellant (59%)59% related to the paper, Propellant (58%)58% related to the paper, Specific impulse (55%)55% related to the paper
View PDF
137 Citations
open accessOpen access Journal Article DOI: 10.1155/2011/214549
Micro- and Nano-Air Vehicles: State of the Art
Luca Petricca, Per Ohlckers, C. Grinde

Abstract:

Micro- and nano air vehicles are defined as “extremely small and ultra-lightweight air vehicle systems” with a maximum wingspan length of 15 cm and a weight less than 20 grams. Here, we provide a review of the current state of the art and identify the challenges of design and fabrication. Different configurations are evaluate... Micro- and nano air vehicles are defined as “extremely small and ultra-lightweight air vehicle systems” with a maximum wingspan length of 15 cm and a weight less than 20 grams. Here, we provide a review of the current state of the art and identify the challenges of design and fabrication. Different configurations are evaluated, such as fixed wings, rotary wings, and flapping wings. The main advantages and drawbacks for each typology are identified and discussed. Special attention is given to rotary-wing vehicles (helicopter concept); including a review of their main structures, such as the airframe, energy storage, controls, and communications systems. In addition, a review of relevant sensors is also included. Examples of existing and future systems are also included. Micro- and nano-vehicles with rotary wings and rechargeable batteries are dominating. The flight times of current systems are typically around 1 hour or less due to the limited energy storage capabilities of the used rechargeable batteries. Fuel cells and ultra capacitors are promising alternative energy supply technologies for the future. Technology improvements, mainly based on micro- and nanotechnologies, are expected to continue in an evolutionary way to improve the capabilities of future micro- and nano air vehicles, giving improved flight times and payload capabilities. read more read less

Topics:

Energy storage (51%)51% related to the paper
View PDF
129 Citations
open accessOpen access Journal Article DOI: 10.1155/2008/732828
Optimal airport surface traffic planning using mixed-integer linear programming
Paul C. Roling1, Hendrikus G. Visser1

Abstract:

We describe an ongoing research effort pertaining to the development of a surface traffic automation system that will help controllers to better coordinate surface traffic movements related to arrival and departure traffic. More specifically, we describe the concept for a taxi-planning support tool that aims to optimize the r... We describe an ongoing research effort pertaining to the development of a surface traffic automation system that will help controllers to better coordinate surface traffic movements related to arrival and departure traffic. More specifically, we describe the concept for a taxi-planning support tool that aims to optimize the routing and scheduling of airport surface traffic in such a way as to deconflict the taxi plans while optimizing delay, total taxi-time, or some other airport efficiency metric. Certain input parameters related to resource demand, such as the expected landing times and the expected pushback times, are rather difficult to predict accurately. Due to uncertainty in the input data driving the taxi-planning process, the taxi-planning tool is designed such that it produces solutions that are robust to uncertainty. The taxi-planning concept presented herein, which is based on mixed-integer linear programming, is designed such that it is able to adapt to perturbations in these input conditions, as well as to account for failure in the actual execution of surface trajectories. The capabilities of the tool are illustrated in a simple hypothetical airport. read more read less

Topics:

Integer programming (53%)53% related to the paper, Linear programming (51%)51% related to the paper
View PDF
120 Citations
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International Journal of Aerospace Engineering format uses unsrt citation style.

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Frequently asked questions

1. Can I write International Journal of Aerospace Engineering in LaTeX?

Absolutely not! Our tool has been designed to help you focus on writing. You can write your entire paper as per the International Journal of Aerospace Engineering guidelines and auto format it.

2. Do you follow the International Journal of Aerospace Engineering guidelines?

Yes, the template is compliant with the International Journal of Aerospace Engineering guidelines. Our experts at SciSpace ensure that. If there are any changes to the journal's guidelines, we'll change our algorithm accordingly.

3. Can I cite my article in multiple styles in International Journal of Aerospace Engineering?

Of course! We support all the top citation styles, such as APA style, MLA style, Vancouver style, Harvard style, and Chicago style. For example, when you write your paper and hit autoformat, our system will automatically update your article as per the International Journal of Aerospace Engineering citation style.

4. Can I use the International Journal of Aerospace Engineering templates for free?

Sign up for our free trial, and you'll be able to use all our features for seven days. You'll see how helpful they are and how inexpensive they are compared to other options, Especially for International Journal of Aerospace Engineering.

5. Can I use a manuscript in International Journal of Aerospace Engineering that I have written in MS Word?

Yes. You can choose the right template, copy-paste the contents from the word document, and click on auto-format. Once you're done, you'll have a publish-ready paper International Journal of Aerospace Engineering that you can download at the end.

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7. Where can I find the template for the International Journal of Aerospace Engineering?

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8. Can I reformat my paper to fit the International Journal of Aerospace Engineering's guidelines?

Of course! You can do this using our intuitive editor. It's very easy. If you need help, our support team is always ready to assist you.

9. International Journal of Aerospace Engineering an online tool or is there a desktop version?

SciSpace's International Journal of Aerospace Engineering is currently available as an online tool. We're developing a desktop version, too. You can request (or upvote) any features that you think would be helpful for you and other researchers in the "feature request" section of your account once you've signed up with us.

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After writing your paper autoformatting in International Journal of Aerospace Engineering, you can download it in multiple formats, viz., PDF, Docx, and LaTeX.

12. Is International Journal of Aerospace Engineering's impact factor high enough that I should try publishing my article there?

To be honest, the answer is no. The impact factor is one of the many elements that determine the quality of a journal. Few of these factors include review board, rejection rates, frequency of inclusion in indexes, and Eigenfactor. You need to assess all these factors before you make your final call.

13. What is Sherpa RoMEO Archiving Policy for International Journal of Aerospace Engineering?

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 Aerospace Engineering. 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 Aerospace Engineering?

The 5 most common citation types in order of usage for International Journal of Aerospace Engineering are:.

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

15. How do I submit my article to the International Journal of Aerospace Engineering?

It is possible to find the Word template for any journal on Google. However, why use a template when you can write your entire manuscript on SciSpace , auto format it as per International Journal of Aerospace Engineering's guidelines and download the same in Word, PDF and LaTeX formats? Give us a try!.

16. Can I download International Journal of Aerospace Engineering in Endnote format?

Yes, SciSpace provides this functionality. After signing up, you would need to import your existing references from Word or Bib file to SciSpace. Then SciSpace would allow you to download your references in International Journal of Aerospace Engineering Endnote style according to Elsevier guidelines.

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