Example of Journal of Propulsion and Power format
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Example of Journal of Propulsion and Power format Example of Journal of Propulsion and Power format Example of Journal of Propulsion and Power format Example of Journal of Propulsion and Power format Example of Journal of Propulsion and Power format Example of Journal of Propulsion and Power format Example of Journal of Propulsion and Power format Example of Journal of Propulsion and Power format Example of Journal of Propulsion and Power format Example of Journal of Propulsion and Power format Example of Journal of Propulsion and Power format Example of Journal of Propulsion and Power format Example of Journal of Propulsion and Power format Example of Journal of Propulsion and Power format Example of Journal of Propulsion and Power format Example of Journal of Propulsion and Power format
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open access Open Access

Journal of Propulsion and Power — Template for authors

Categories Rank Trend in last 3 yrs
Aerospace Engineering #16 of 129 up up by 5 ranks
Mechanical Engineering #108 of 596 up up by 12 ranks
Space and Planetary Science #29 of 97 up up by 7 ranks
Fuel Technology #30 of 100 down down by 7 ranks
journal-quality-icon Journal quality:
High
calendar-icon Last 4 years overview: 456 Published Papers | 2354 Citations
indexed-in-icon Indexed in: Scopus
last-updated-icon Last updated: 09/06/2020
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Related Journals

open access Open Access

IEEE

Quality:  
High
CiteRatio: 3.7
SJR: 0.396
SNIP: 1.133
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SAGE

Quality:  
High
CiteRatio: 5.0
SJR: 0.89
SNIP: 1.518
open access Open Access
recommended Recommended

American Institute of Aeronautics and Astronautics

Quality:  
High
CiteRatio: 6.0
SJR: 1.573
SNIP: 1.754

Journal Performance & Insights

Impact Factor

CiteRatio

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.

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

1.94

8% from 2018

Impact factor for Journal of Propulsion and Power from 2016 - 2019
Year Value
2019 1.94
2018 1.803
2017 1.362
2016 1.144
graph view Graph view
table view Table view

5.2

8% from 2019

CiteRatio for Journal of Propulsion and Power from 2016 - 2020
Year Value
2020 5.2
2019 4.8
2018 3.6
2017 3.5
2016 3.2
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.

insights Insights

  • CiteRatio of this journal has increased by 8% in last years.
  • This journal’s CiteRatio is in the top 10 percentile category.

SCImago Journal Rank (SJR)

Source Normalized Impact per Paper (SNIP)

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.

0.913

15% from 2019

SJR for Journal of Propulsion and Power from 2016 - 2020
Year Value
2020 0.913
2019 0.795
2018 0.657
2017 0.665
2016 0.585
graph view Graph view
table view Table view

1.35

6% from 2019

SNIP for Journal of Propulsion and Power from 2016 - 2020
Year Value
2020 1.35
2019 1.433
2018 1.422
2017 1.446
2016 1.269
graph view Graph view
table view Table view

insights Insights

  • SJR of this journal has increased by 15% in last years.
  • This journal’s SJR is in the top 10 percentile category.

insights Insights

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

Journal of Propulsion and Power

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American Institute of Aeronautics and Astronautics

Journal of Propulsion and Power

This Journal is devoted to the advancement of the science and technology of aerospace propulsion and power through the dissemination of original archival papers contributing to advancements in airbreathing, electric, and advanced propulsion; solid and liquid rockets; fuels and...... Read More

Engineering

i
Last updated on
09 Jun 2020
i
ISSN
0748-4658
i
Impact Factor
High - 1.618
i
Open Access
No
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., 97(6):067007, 2006.

Top papers written in this journal

open accessOpen access Journal Article DOI: 10.2514/1.18239
Nickel-Based Superalloys for Advanced Turbine Engines: Chemistry, Microstructure and Properties
Tresa M. Pollock1, Sammy Tin2

Abstract:

The chemical, physical, and mechanical characteristics of nickel-based superalloys are reviewed with emphasis on the use of this class of materials within turbine engines. The role of major and minor alloying additions in multicomponent commercial cast and wrought superalloys is discussed. Microstructural stability and phases... The chemical, physical, and mechanical characteristics of nickel-based superalloys are reviewed with emphasis on the use of this class of materials within turbine engines. The role of major and minor alloying additions in multicomponent commercial cast and wrought superalloys is discussed. Microstructural stability and phases observed during processing and in subsequent elevated-temperature service are summarized. Processing paths and recent advances in processing are addressed. Mechanical properties and deformation mechanisms are reviewed, including tensile properties, creep, fatigue, and cyclic crack growth. I. Introduction N ICKEL-BASED superalloys are an unusual class of metallic materials with an exceptional combination of hightemperature strength, toughness, and resistance to degradation in corrosive or oxidizing environments. These materials are widely used in aircraft and power-generation turbines, rocket engines, and other challenging environments, including nuclear power and chemical processing plants. Intensive alloy and process development activities during the past few decades have resulted in alloys that can tolerate average temperatures of 1050 ◦ C with occasional excursions (or local hot spots near airfoil tips) to temperatures as high as 1200 ◦ C, 1 which is approximately 90% of the melting point of the material. The underlying aspects of microstructure and composition that result in these exceptional properties are briefly reviewed here. Major classes of superalloys that are utilized in gas-turbine engines and the corresponding processes for their production are outlined along with characteristic mechanical and physical properties. read more read less

Topics:

Turbine blade (53%)53% related to the paper, Creep (51%)51% related to the paper, Superalloy (51%)51% related to the paper
View PDF
1,826 Citations
Journal Article DOI: 10.2514/1.18034
Gas Turbine Film Cooling
David G. Bogard1, Karen A. Thole2

Abstract:

The durability of gas turbine engines is strongly dependent on the component temperatures. For the combustor and turbine airfoils and endwalls, film cooling is used extensively to reduce component temperatures. Film cooling is a cooling method used in virtually all of today's aircraft turbine engines and in many power-generat... The durability of gas turbine engines is strongly dependent on the component temperatures. For the combustor and turbine airfoils and endwalls, film cooling is used extensively to reduce component temperatures. Film cooling is a cooling method used in virtually all of today's aircraft turbine engines and in many power-generation turbine engines and yet has very difficult phenomena to predict. The interaction of jets-in-crossflow, which is representative of film cooling, results in a shear layer that leads to mixing and a decay in the cooling performance along a surface. This interaction is highly dependent on the jet-to-crossflow mass and momentum flux ratios. Film-cooling performance is difficult to predict because of the inherent complex flowfields along the airfoil component surfaces in turbine engines. Film cooling is applied to nearly all of the external surfaces associated with the airfoils that are exposed to the hot combustion gasses such as the leading edges, main bodies, blade tips, and endwalls. In a review of the literature, it was found that there are strong effects of freestream turbulence, surface curvature, and hole shape on the performance of film cooling. Film cooling is reviewed through a discussion of the analyses methodologies, a physical description, and the various influences on film-cooling performance. read more read less

Topics:

Turbine blade (63%)63% related to the paper, Turbine (60%)60% related to the paper, Combustor (57%)57% related to the paper
636 Citations
Journal Article DOI: 10.2514/1.17656
Continuous Spin Detonations
F. A. Bykovskii1, S. A. Zhdan1, Evgenii F. Vedernikov1

Abstract:

Results on controlled continuous spin detonation of various fuels in liquid-propellant rocket motors and ramjet combustors are reported. Schemes of chambers, combustion in transverse detonation waves, and typical photographic records of transverse detonation waves are given. The flow structure, existence conditions, and basic... Results on controlled continuous spin detonation of various fuels in liquid-propellant rocket motors and ramjet combustors are reported. Schemes of chambers, combustion in transverse detonation waves, and typical photographic records of transverse detonation waves are given. The flow structure, existence conditions, and basic properties of continuous detonation are considered. An analysis of physical, chemical, and geometric parameters determining spin detonation is presented. Results of studying continuous spin detonation of C 2 H 2 + air and H 2 + air mixtures in an annular ducted chamber 30.6 cm in diameter are reported. The range of existence of continuous spin detonation in fuel-air mixtures is determined as a function of the governing parameters. In the case of high-quality mixing, the transverse detonation wave velocity and structure are extremely stable in a wide range of the ratios of propellant components and in the examined range of pressures in the chamber. read more read less

Topics:

Detonation (74%)74% related to the paper, Deflagration to detonation transition (71%)71% related to the paper, Pulse detonation engine (63%)63% related to the paper, Chapman–Jouguet condition (61%)61% related to the paper, Propellant (54%)54% related to the paper
621 Citations
Journal Article DOI: 10.2514/2.5875
Scramjet Engines: The First Forty Years
Edward T. Curran1

Abstract:

Ageneralreviewoftheemergenceandmaturingofsupersoniccombustionramjet (scramjet)enginetechnologies overthelast 40 years is presented. The review isgiven in terms of theeffortscompleted or proceeding in theUnited States, Russia, France, Germany, Japan, Australia, and other countries. A brief account of the challenges of scramjet... Ageneralreviewoftheemergenceandmaturingofsupersoniccombustionramjet (scramjet)enginetechnologies overthelast 40 years is presented. The review isgiven in terms of theeffortscompleted or proceeding in theUnited States, Russia, France, Germany, Japan, Australia, and other countries. A brief account of the challenges of scramjet combustor development is given, and attention is directed toward other source references for more detailed accounts of technology evolution. Two emerging scramjet applications are identie ed, namely, hydrogenfueledhigh-speed engines foraccess to spaceand hydrocarbon-fueled enginesforhypersonicair-launched missiles. read more read less

Topics:

Scramjet (54%)54% related to the paper, Combustor (53%)53% related to the paper
602 Citations
Journal Article DOI: 10.2514/2.5818
Cavity Flame-Holders for Ignition and Flame Stabilization in Scramjets: An Overview
Adela Ben-Yakar1, Ronald K. Hanson1

Abstract:

This paper describes ongoing research efforts in the scramjet community on cavity e ame holders, a concept for e ame holding and stabilization in supersonic combustors. During the last few years, cavities have gained the attention of the scramjet community as a promising e ame-holding device, owing to results obtained in e ig... This paper describes ongoing research efforts in the scramjet community on cavity e ame holders, a concept for e ame holding and stabilization in supersonic combustors. During the last few years, cavities have gained the attention of the scramjet community as a promising e ame-holding device, owing to results obtained in e ight tests and to feasibility demonstrations in laboratory-scale supersonic combustors. However, comprehensive studies are needed to determine the optimal cone guration that will yield the most effective e ame-holding capability with minimum losses. The e owe eld characteristics of cavities and research efforts related to cavities employed in lowand high-speed e ows are summarized. Open questions impacting the effectiveness of the cavities as e ame holders in supersonic combustors are discussed. read more read less

Topics:

Scramjet (52%)52% related to the paper
View PDF
590 Citations
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Journal of Propulsion and Power format uses unsrt citation style.

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Frequently asked questions

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

2. Do you follow the Journal of Propulsion and Power guidelines?

Yes, the template is compliant with the Journal of Propulsion and Power 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 Propulsion and Power?

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 Propulsion and Power citation style.

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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 Propulsion and Power.

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

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7. Where can I find the template for the Journal of Propulsion and Power?

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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.

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SciSpace's Journal of Propulsion and Power 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 Journal of Propulsion and Power, you can download it in multiple formats, viz., PDF, Docx, and LaTeX.

12. Is Journal of Propulsion and Power'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 Propulsion and Power?

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 Propulsion and Power. 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 Propulsion and Power?

The 5 most common citation types in order of usage for Journal of Propulsion and Power 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 Propulsion and Power?

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16. Can I download Journal of Propulsion and Power 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 Propulsion and Power Endnote style according to Elsevier guidelines.

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