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Journal of Propulsion and Power is a peer-reviewed journal published by AIAA, covering Rocket and propulsion systems research, Computational Fluid Dynamics and Aerodynamics, Combustion and flame dynamics. Over its lifetime it has published 6,156 papers, which have received 164,243 citations.
| Publisher | AIAA |
|---|---|
| Reference style | Numbered (AIAA) Numbered — [1], [2] in the text [1] Smith, A., Jones, B., and Lee, C., "A Representative Article Title," Journal of Propulsion and Power, Vol. 12, No. 3, 2023, pp. 45–58.
Formats any DOI in Journal of Propulsion and Power style. No sign-up. |
| Publishes research in | Rocket and propulsion systems research Computational Fluid Dynamics and Aerodynamics Combustion and flame dynamics Energetic Materials and Combustion Fluid Dynamics and Turbulent Flows |
| ISSN | 0748-4658 |
| Citation impact (2-yr) | 2.71 |
| h-index | 138 |
| i10-index | 3,589 |
| Top institutions publishing here | Glenn Research Center |
| Journal website | www.catchword.com |
| You get | A submission-ready PDF and the editable LaTeX source — ready to submit. |
Citations each year’s papers have accumulated so far — the most recent years are still building up.
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.…
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…
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…
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…
This paper describes ongoing research efforts in the scramjet community on cavity ame holders, a concept for ame holding and stabilization in supersonic combustors. During the last few years, cavities have gained the attention of the scramjet community as a promising ame-holding device, owing to results obtained in ight tests and to feasibility demonstrations in…
