Example of Journal of Aircraft format
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Example of Journal of Aircraft format Example of Journal of Aircraft format Example of Journal of Aircraft format Example of Journal of Aircraft format Example of Journal of Aircraft format Example of Journal of Aircraft format Example of Journal of Aircraft format Example of Journal of Aircraft format Example of Journal of Aircraft format Example of Journal of Aircraft format Example of Journal of Aircraft format Example of Journal of Aircraft format Example of Journal of Aircraft format Example of Journal of Aircraft format Example of Journal of Aircraft format
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Example of Journal of Aircraft format Example of Journal of Aircraft format Example of Journal of Aircraft format Example of Journal of Aircraft format Example of Journal of Aircraft format Example of Journal of Aircraft format Example of Journal of Aircraft format Example of Journal of Aircraft format Example of Journal of Aircraft format Example of Journal of Aircraft format Example of Journal of Aircraft format Example of Journal of Aircraft format Example of Journal of Aircraft format Example of Journal of Aircraft format Example of Journal of Aircraft format
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open access Open Access

Journal of Aircraft — Template for authors

Categories Rank Trend in last 3 yrs
Aerospace Engineering #28 of 129 down down by 1 rank
journal-quality-icon Journal quality:
High
calendar-icon Last 4 years overview: 703 Published Papers | 2732 Citations
indexed-in-icon Indexed in: Scopus
last-updated-icon Last updated: 15/07/2020
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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.

3.9

30% from 2019

CiteRatio for Journal of Aircraft from 2016 - 2020
Year Value
2020 3.9
2019 3.0
2018 2.8
2017 2.9
2016 2.9
graph view Graph view
table view Table view

0.64

28% from 2019

SJR for Journal of Aircraft from 2016 - 2020
Year Value
2020 0.64
2019 0.499
2018 0.409
2017 0.388
2016 0.49
graph view Graph view
table view Table view

1.008

25% from 2019

SNIP for Journal of Aircraft from 2016 - 2020
Year Value
2020 1.008
2019 1.346
2018 1.229
2017 1.194
2016 1.434
graph view Graph view
table view Table view

insights Insights

  • CiteRatio of this journal has increased by 30% in last years.
  • This journal’s CiteRatio is in the top 10 percentile category.

insights Insights

  • SJR of this journal has increased by 28% in last years.
  • This journal’s SJR is in the top 10 percentile category.

insights Insights

  • SNIP of this journal has decreased by 25% in last years.
  • This journal’s SNIP is in the top 10 percentile category.

Journal of Aircraft

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American Institute of Aeronautics and Astronautics

Journal of Aircraft

This Journal is devoted to the advancement of the applied science and technology of airborne flight through the dissemination of original archival papers describing significant advances in aircraft, the operation of aircraft, and applications of aircraft technology to other fi...... Read More

Engineering

i
Last updated on
14 Jul 2020
i
ISSN
0021-8669
i
Impact Factor
High - 1.68
i
Open Access
No
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Sherpa RoMEO Archiving Policy
Green faq
i
Plagiarism Check
Available via Turnitin
i
Endnote Style
Download Available
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Bibliography Name
unsrt
i
Citation Type
Numbered
[25]
i
Bibliography Example
C. W. J. Beenakker. Specular andreev reflection in graphene. Phys. Rev. Lett., 97(6):067007, 2006.

Top papers written in this journal

Journal Article DOI: 10.2514/3.58379
Wing Design by Numerical Optimization
Raymond M. Hicks1, Preston A. Henne2
01 Aug 1977 - Journal of Aircraft

Abstract:

A study was conducted to assess the feasibility of performing computerized wing design by numerical optimization. The design program combined a full potential, inviscid aerodynamics code with a conjugate gradient optimization algorithm. Three design problems were selected to demonstrate the design technique. The first involve... A study was conducted to assess the feasibility of performing computerized wing design by numerical optimization. The design program combined a full potential, inviscid aerodynamics code with a conjugate gradient optimization algorithm. Three design problems were selected to demonstrate the design technique. The first involved modifying the upper surface of the inboard 50% of a swept wing to reduce the shock drag subject to a constraint on wing volume. The second involved modifying the entire upper surface of the same swept wing (except the tip section) to increase the lift-drag ratio subject to constraints on wing volume and lift coefficient. The final problem involved modifying the inboard 50% of a low-speed wing to achieve good stall progression. Results from the three cases indicate that the technique is sufficiently accurate to permit substantial improvement in the design objectives. read more read less

Topics:

Angle of attack (62%)62% related to the paper, Lift-to-drag ratio (61%)61% related to the paper, Swept wing (61%)61% related to the paper, Wing (55%)55% related to the paper, Airfoil (54%)54% related to the paper
984 Citations
Journal Article DOI: 10.2514/3.44330
Interpolation using surface splines.
Robert L. Harder, Robert N. Desmarais1
01 Feb 1972 - Journal of Aircraft

Abstract:

A surface spline is a mathematical tool for interpolating a function of two variables. It is based upon the small deflection equation of an infinite plate. The surface spline depends upon the solution of a system of linear equations, and thus, will ordinarily require the use of a digital computer. The closed form solution inv... A surface spline is a mathematical tool for interpolating a function of two variables. It is based upon the small deflection equation of an infinite plate. The surface spline depends upon the solution of a system of linear equations, and thus, will ordinarily require the use of a digital computer. The closed form solution involves no functions more complicated than logarithms, and is easily coded. Several modifications which can be incorporated are discussed. read more read less

Topics:

Spline interpolation (68%)68% related to the paper, Polyharmonic spline (65%)65% related to the paper, Thin plate spline (65%)65% related to the paper, Box spline (61%)61% related to the paper, Interpolation (57%)57% related to the paper
753 Citations
Journal Article DOI: 10.2514/3.45534
Progress in analysis and prediction of dynamic stall
Lawrence W. Carr1
01 Jan 1988 - Journal of Aircraft

Abstract:

Nomenclature c = chord CD =drag coefficient, D/qA CL =lift coefficient, L/qa CP = pressure coefficient, P-PW /q CM = pitching-moment coefficient, M/qA D =drag, Ib k = reduced frequency, wc/2U L =lift, Ib M =Mach number; pitching moment, ft-lb P = pressure, lb/in q = dynamic pressure, 1 /2p U R, Re, Re, Rn = Reynolds number t ... Nomenclature c = chord CD =drag coefficient, D/qA CL =lift coefficient, L/qa CP = pressure coefficient, P-PW /q CM = pitching-moment coefficient, M/qA D =drag, Ib k = reduced frequency, wc/2U L =lift, Ib M =Mach number; pitching moment, ft-lb P = pressure, lb/in q = dynamic pressure, 1 /2p U R, Re, Re, Rn = Reynolds number t time U,V = freestream velocity, ft/s x = distance a = angle of attack, deg f =nondimensional chord length, x/c $tr transition location co = rotational frequency, rad/s p = density, lb/ft A = sweep angle, deg read more read less

Topics:

Lift coefficient (58%)58% related to the paper, Pressure coefficient (53%)53% related to the paper, Drag (51%)51% related to the paper, Drag coefficient (51%)51% related to the paper, Angle of attack (50%)50% related to the paper
689 Citations
Journal Article DOI: 10.2514/3.47003
Delay of Airfoil Stall by Periodic Excitation
Avi Seifert1, A. Darabi1, Israel Wygnanski
01 Jul 1996 - Journal of Aircraft

Abstract:

It was recently demonstrated that oscillatory blowing can delay separation from a symmetrical airfoil much more effectively than the steady blowing used traditionally for this purpose. Experiments carried out on different airfoils revealed that this flow depends on many parameters such as, the location of the blowing slot, th... It was recently demonstrated that oscillatory blowing can delay separation from a symmetrical airfoil much more effectively than the steady blowing used traditionally for this purpose. Experiments carried out on different airfoils revealed that this flow depends on many parameters such as, the location of the blowing slot, the steady and oscillatory momentum coefficients of the jet, the frequency of imposed oscillations, and the shape and incidence of the particular airfoil. In airfoils equipped with slotted flaps, the flow is also dependent on the geometry of the slot and on the Reynolds number in addition to the flap deflection that is considered as a part of the airfoil shape. The incremental improvements in single element airfoil characteristics are generally insensitive to a change in Reynolds number, provided the latter is sufficiently large. The imposed oscillations do not generate large oscillatory lift nor do they cause a periodic meander of the c.p. C* C D = dp Ct = read more read less

Topics:

Airfoil (61%)61% related to the paper, Lift coefficient (57%)57% related to the paper, Reynolds number (54%)54% related to the paper, Stall (fluid mechanics) (53%)53% related to the paper, Adverse pressure gradient (52%)52% related to the paper
669 Citations
open accessOpen access Journal Article DOI: 10.2514/1.9084
Design of the Blended Wing Body Subsonic Transport
01 Jan 2004 - Journal of Aircraft

Abstract:

The Boeing Blended-Wing-Body (BWB) airplane concept represents a potential breakthrough in subsonic transport efficiency. Work began on this concept via a study to demonstrate feasibility and begin development of this new class of airplane. In this initial study, 800-passenger BWB and conventional configuration airplanes were... The Boeing Blended-Wing-Body (BWB) airplane concept represents a potential breakthrough in subsonic transport efficiency. Work began on this concept via a study to demonstrate feasibility and begin development of this new class of airplane. In this initial study, 800-passenger BWB and conventional configuration airplanes were sized and compared for a 7000-n mile design range. Both airplanes were based on engine and structural (composite) technology for a 2010 entry into service read more read less

Topics:

Airplane (54%)54% related to the paper
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641 Citations
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Journal of Aircraft format uses unsrt citation style.

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Frequently asked questions

1. Can I write Journal of Aircraft in LaTeX?

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

2. Do you follow the Journal of Aircraft guidelines?

Yes, the template is compliant with the Journal of Aircraft 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 Journal of Aircraft?

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 Journal of Aircraft citation style.

4. Can I use the Journal of Aircraft 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 Journal of Aircraft.

5. Can I use a manuscript in Journal of Aircraft 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 Journal of Aircraft that you can download at the end.

6. How long does it usually take you to format my papers in Journal of Aircraft?

It only takes a matter of seconds to edit your manuscript. Besides that, our intuitive editor saves you from writing and formatting it in Journal of Aircraft.

7. Where can I find the template for the Journal of Aircraft?

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 Journal of Aircraft's guidelines and download the same in Word, PDF and LaTeX formats? Give us a try!.

8. Can I reformat my paper to fit the Journal of Aircraft'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. Journal of Aircraft an online tool or is there a desktop version?

SciSpace's Journal of Aircraft 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.

10. I cannot find my template in your gallery. Can you create it for me like Journal of Aircraft?

Sure. You can request any template and we'll have it setup within a few days. You can find the request box in Journal Gallery on the right side bar under the heading, "Couldn't find the format you were looking for like Journal of Aircraft?”

11. What is the output that I would get after using Journal of Aircraft?

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

12. Is Journal of Aircraft'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 Journal of Aircraft?

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 Journal of Aircraft. 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 Journal of Aircraft?

The 5 most common citation types in order of usage for Journal of Aircraft 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 Journal of Aircraft?

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16. Can I download Journal of Aircraft 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 Journal of Aircraft Endnote style according to Elsevier guidelines.

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