Example of AIAA Journal format
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Example of AIAA Journal format Example of AIAA Journal format Example of AIAA Journal format Example of AIAA Journal format Example of AIAA Journal format Example of AIAA Journal format Example of AIAA Journal format Example of AIAA Journal format Example of AIAA Journal format Example of AIAA Journal format Example of AIAA Journal format Example of AIAA Journal format Example of AIAA Journal format Example of AIAA Journal format Example of AIAA Journal format Example of AIAA Journal format Example of AIAA Journal format Example of AIAA Journal format Example of AIAA Journal format Example of AIAA Journal format Example of AIAA Journal format
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Example of AIAA Journal format Example of AIAA Journal format Example of AIAA Journal format Example of AIAA Journal format Example of AIAA Journal format Example of AIAA Journal format Example of AIAA Journal format Example of AIAA Journal format Example of AIAA Journal format Example of AIAA Journal format Example of AIAA Journal format Example of AIAA Journal format Example of AIAA Journal format Example of AIAA Journal format Example of AIAA Journal format Example of AIAA Journal format Example of AIAA Journal format Example of AIAA Journal format Example of AIAA Journal format Example of AIAA Journal format Example of AIAA Journal format
Sample paper formatted on SciSpace - SciSpace
This content is only for preview purposes. The original open access content can be found here.
open access Open Access ISSN: 11452 e-ISSN: 1533385X

AIAA Journal — Template for authors

Categories Rank Trend in last 3 yrs
Aerospace Engineering #19 of 129 down down by 3 ranks
journal-quality-icon Journal quality:
High
calendar-icon Last 4 years overview: 1648 Published Papers | 8209 Citations
indexed-in-icon Indexed in: Scopus
last-updated-icon Last updated: 01/07/2020
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General info
Top papers
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FAQ

Journal Performance & Insights

  • Impact Factor
  • CiteRatio
  • SJR
  • SNIP

Impact factor determines the importance of a journal by taking a measure of frequency with which the average article in a journal has been cited in a particular year.

2.108

8% from 2018

Impact factor for AIAA Journal from 2016 - 2019
Year Value
2019 2.108
2018 1.951
2017 1.556
2016 1.638
graph view Graph view
table view Table view

insights Insights

  • Impact factor of this journal has increased by 8% in last year.
  • This journal’s impact factor is in the top 10 percentile category.

CiteRatio is a measure of average citations received per peer-reviewed paper published in the journal.

5.0

16% from 2019

CiteRatio for AIAA Journal from 2016 - 2020
Year Value
2020 5.0
2019 4.3
2018 4.2
2017 3.9
2016 4.2
graph view Graph view
table view Table view

insights Insights

  • CiteRatio of this journal has increased by 16% in last years.
  • This journal’s CiteRatio is in the top 10 percentile category.

SCImago Journal Rank (SJR) measures weighted citations received by the journal. Citation weighting depends on the categories and prestige of the citing journal.

0.828

4% from 2019

SJR for AIAA Journal from 2016 - 2020
Year Value
2020 0.828
2019 0.866
2018 0.783
2017 0.763
2016 0.857
graph view Graph view
table view Table view

insights Insights

  • SJR of this journal has decreased by 4% in last years.
  • This journal’s SJR is in the top 10 percentile category.

Source Normalized Impact per Paper (SNIP) measures actual citations received relative to citations expected for the journal's category.

1.386

2% from 2019

SNIP for AIAA Journal from 2016 - 2020
Year Value
2020 1.386
2019 1.42
2018 1.607
2017 1.467
2016 1.721
graph view Graph view
table view Table view

insights Insights

  • SNIP of this journal has decreased by 2% in last years.
  • This journal’s SNIP is in the top 10 percentile category.

Related Journals

open access Open Access ISSN: 8858985

IEEE

CiteRatio: 3.7 | SJR: 0.396 | SNIP: 1.133
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recommended Recommended

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CiteRatio: 7.5 | SJR: 1.137 | SNIP: 2.134
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CiteRatio: 6.8 | SJR: 1.321 | SNIP: 1.764
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CiteRatio: 10.9 | SJR: 1.365 | SNIP: 2.086

AIAA Journal

Guideline source: View

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American Institute of Aeronautics and Astronautics

AIAA Journal

This Journal is devoted to the advancement of the science and technology of astronautics and aeronautics through the dissemination of original archival research papers disclosing new theoretical developments and/or experimental results. The topics include aeroacoustics, aerody...... Read More

Engineering

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Last updated on
01 Jul 2020
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ISSN
0001-1452
i
Impact Factor
High - 1.868
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Open Access
No
i
Sherpa RoMEO Archiving Policy
Green faq
i
Plagiarism Check
Available via Turnitin
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Endnote Style
Download Available
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Bibliography Name
unsrt
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Citation Type
Numbered
[25]
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Bibliography Example
Blonder G.E., Tinkham M., and Klapwijk T.M., “Transition from metallic to tunneling regimes in superconducting micro-constrictions: Excess current, charge imbalance, and supercurrent conversion,” Phys. Rev. B , vol. 25, no. 7, pp. 4515–4532,1982.

Top papers written in this journal

open accessOpen access Journal Article DOI: 10.2514/3.12149
Two-equation eddy-viscosity turbulence models for engineering applications
Florian R. Menter1
01 Aug 1994 - AIAA Journal

Abstract:

Two new two-equation eddy-viscosity turbulence models will be presented. They combine different elements of existing models that are considered superior to their alternatives. The first model, referred to as the baseline (BSL) model, utilizes the original k-ω model of Wilcox in the inner region of the boundary layer and switc... Two new two-equation eddy-viscosity turbulence models will be presented. They combine different elements of existing models that are considered superior to their alternatives. The first model, referred to as the baseline (BSL) model, utilizes the original k-ω model of Wilcox in the inner region of the boundary layer and switches to the standard k-e model in the outer region and in free shear flows. It has a performance similar to the Wilcox model, but avoids that model's strong freestream sensitivity read more read less

Topics:

K-epsilon turbulence model (65%)65% related to the paper, Spalart–Allmaras turbulence model (62%)62% related to the paper, Turbulence modeling (60%)60% related to the paper, Transition modeling (55%)55% related to the paper, Direct numerical simulation (53%)53% related to the paper
View PDF
12,746 Citations
Journal Article DOI: 10.2514/3.8284
Numerical Study of the Turbulent Flow Past an Airfoil with Trailing Edge Separation
C. M. Rhie1, W. L. Chow2
01 Nov 1983 - AIAA Journal

Abstract:

Presentation d'une methode numerique par volume fini pour la resolution des equations de Navier-Stokes bidimensionnelles, incompressibles, et stationnaires, en coordonnees generales curvilignes Application de la methode aux ecoulements turbulents sur des profils avec et sans separation au bord de sortie posterieur Comparaison... Presentation d'une methode numerique par volume fini pour la resolution des equations de Navier-Stokes bidimensionnelles, incompressibles, et stationnaires, en coordonnees generales curvilignes Application de la methode aux ecoulements turbulents sur des profils avec et sans separation au bord de sortie posterieur Comparaison des calculs avec des donnees experimentales read more read less
4,104 Citations
open accessOpen access Journal Article DOI: 10.2514/3.4741
Coupling of substructures for dynamic analyses.
M. C. C. Bampton, Roy R. Craig1
01 Jul 1968 - AIAA Journal

Abstract:

A method for treating a complex structure as an assemblage of distinct regions, or substructures, is presented. Using basic mass and stiffness matrices for the substructures, together with conditions of geometrical compatibility along substructure boundaries, the method employs two forms of generalized coordinates. Boundary g... A method for treating a complex structure as an assemblage of distinct regions, or substructures, is presented. Using basic mass and stiffness matrices for the substructures, together with conditions of geometrical compatibility along substructure boundaries, the method employs two forms of generalized coordinates. Boundary generalized coordinates give displacements and rotations of points along substructure boundaries and are related to the displacement modes of the substructures known as "constraint modes." All constraint modes are generated by matrix operations from substructure input data. Substructure normal-mode generalized coordinates are related to free vibration modes of the substructures relative to completely restrained boundaries. The definition of substructure modes and the requirement of compatibility along substructure boundaries lead to coordinate transformation matrices that are employed in obtaining system mass and stiffness matrices from the mass and stiffness matrices of the substructures. Provision is made, through a RayleighRitz procedure, for reducing the total number of degrees of freedom of a structure while retaining accurate description of its dynamic behavior. Substructure boundaries may have any degree of redundancy. An example is presented giving a free vibration analysis of a structure having a highly indeterminate substructure boundary. read more read less

Topics:

Substructure (58%)58% related to the paper, Generalized coordinates (55%)55% related to the paper, Dynamic substructuring (53%)53% related to the paper, Coordinate system (51%)51% related to the paper
View PDF
2,821 Citations
Journal Article DOI: 10.2514/3.9792
Use of piezoelectric actuators as elements of intelligent structures
Edward F. Crawley1, Javier de Luis1
01 Oct 1987 - AIAA Journal

Abstract:

This work presents the analytic and experimental development of piezoelectric actuators as elements of intelligent structures, i.e., structures with highly distributed actuators, sensors, and processing networks. Static and dynamic analytic models are derived for segmented piezoelectric actuators that are either bonded to an ... This work presents the analytic and experimental development of piezoelectric actuators as elements of intelligent structures, i.e., structures with highly distributed actuators, sensors, and processing networks. Static and dynamic analytic models are derived for segmented piezoelectric actuators that are either bonded to an elastic substructure or embedded in a laminated composite. These models lead to the ability to predict, a priori, the response of the structural member to a command voltage applied to the piezoelectric and give guidance as to the optimal location for actuator placement. A scaling analysis is performed to demonstrate that the effectiveness of piezoelectric actuators is independent of the size of the structure and to evaluate various piezoelectric materials based on their effectiveness in transmitting strain to the substructure. Three test specimens of cantilevered beams were constructed: an aluminum beam with surface-bonded actuators, a glass/epoxy beam with embedded actuators, and a graphite/epoxy beam with embedded actuators. The actuators were used to excite steady-state resonant vibrations in the cantilevered beams. The response of the specimens compared well with those predicted by the analytic models. Static tensile tests performed on glass/epoxy laminates indicated that the embedded actuator reduced the ultimate strength of the laminate by 20%, while not significantly affecting the global elastic modulus of the specimen. read more read less

Topics:

Piezoelectricity (54%)54% related to the paper, Actuator (51%)51% related to the paper, Beam (structure) (50%)50% related to the paper
2,648 Citations
Journal Article DOI: 10.2514/3.10041
Reassessment of the scale-determining equation for advanced turbulence models
01 Nov 1988 - AIAA Journal

Abstract:

A comprehensive and critical review of closure approximations for two-equation turbulence models has been made. Particular attention has focused on the scale-determining equation in an attempt to find the optimum choice of dependent variable and closure approximations. Using a combination of singular perturbation methods and ... A comprehensive and critical review of closure approximations for two-equation turbulence models has been made. Particular attention has focused on the scale-determining equation in an attempt to find the optimum choice of dependent variable and closure approximations. Using a combination of singular perturbation methods and numerical computations, this paper demonstrates that: 1) conventional A:-e and A>w formulations generally are inaccurate for boundary layers in adverse pressure gradient; 2) using "wall functions'' tends to mask the shortcomings of such models; and 3) a more suitable choice of dependent variables exists that is much more accurate for adverse pressure gradient. Based on the analysis, a two-equation turbulence model is postulated that is shown to be quite accurate for attached boundary layers in adverse pressure gradient, compressible boundary layers, and free shear flows. With no viscous damping of the model's closure coefficients and without the aid of wall functions, the model equations can be integrated through the viscous sublayer. Surface boundary conditions are presented that permit accurate predictions for flow over rough surfaces and for flows with surface mass addition. read more read less

Topics:

K-omega turbulence model (61%)61% related to the paper, K-epsilon turbulence model (61%)61% related to the paper, Turbulence modeling (59%)59% related to the paper, Adverse pressure gradient (58%)58% related to the paper, Boundary value problem (57%)57% related to the paper
2,541 Citations
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With SciSpace, you do not need a word template for AIAA Journal.

It automatically formats your research paper to American Institute of Aeronautics and Astronautics formatting guidelines and citation style.

You can download a submission ready research paper in pdf, LaTeX and docx formats.

Time comparison

Time taken to format a paper and Compliance with guidelines

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AIAA Journal format uses unsrt citation style.

Automatically format and order your citations and bibliography in a click.

SciSpace allows imports from all reference managers like Mendeley, Zotero, Endnote, Google Scholar etc.

Frequently asked questions

Absolutely not! With our tool, you can freely write without having to focus on LaTeX. You can write your entire paper as per the AIAA Journal guidelines and autoformat it.

Yes. The template is fully compliant as per the guidelines of this journal. Our experts at SciSpace ensure that. Also, if there's any update in the journal format guidelines, we take care of it and include that in our algorithm.

Sure. We support all the top citation styles like APA style, MLA style, Vancouver style, Harvard style, Chicago style, etc. For example, in case of this journal, when you write your paper and hit autoformat, it will automatically update your article as per the AIAA Journal citation style.

You can avail our Free Trial for 7 days. I'm sure you'll find our features very helpful. Plus, it's quite inexpensive.

Yup. You can choose the right template, copy-paste the contents from the word doc and click on auto-format. You'll have a publish-ready paper that you can download at the end.

A matter of seconds. Besides that, our intuitive editor saves a load of your time in writing and formating your manuscript.

One little Google search can get you the Word template for any journal. However, why do you need a Word template when you can write your entire manuscript on SciSpace, autoformat it as per AIAA Journal's guidelines and download the same in Word, PDF and LaTeX formats? Try us out!.

Absolutely! You can do it using our intuitive editor. It's very easy. If you need help, you can always contact our support team.

SciSpace is an online tool for now. We'll soon release a desktop version. You can also request (or upvote) any feature that you think might be helpful for you and the research community in the feature request section once you sign-up with us.

Sure. You can request any template and we'll have it up and running within a matter of 3 working days. You can find the request box in the Journal Gallery on the right sidebar under the heading, "Couldn't find the format you were looking for?".

After you have written and autoformatted your paper, you can download it in multiple formats, viz., PDF, Docx and LaTeX.

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 those factors the review board, rejection rates, frequency of inclusion in indexes, Eigenfactor, etc. You must assess all the factors and then take the final call.

SHERPA/RoMEO Database

We have extracted this data from Sherpa Romeo to help our researchers understand the access level of this journal. The following table indicates the level of access a journal has as per Sherpa Romeo 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.

The 5 most common citation types in order of usage are:.

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

Our journal submission experts are skilled in submitting papers to various international journals.

After uploading your paper on SciSpace, you would see a button to request a journal submission service for AIAA Journal.

Each submission service is completed within 4 - 5 working days.

Yes. SciSpace provides this functionality.

After signing up, you would need to import your existing references from Word or .bib file.

SciSpace would allow download of your references in AIAA Journal Endnote style, according to american-institute-of-aeronautics-and-astronautics guidelines.

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I spent hours with MS word for reformatting. It was frustrating - plain and simple. With SciSpace, I can draft my manuscripts and once it is finished I can just submit. In case, I have to submit to another journal it is really just a button click instead of an afternoon of reformatting.

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