Write in a clean editor, then format for Jet propulsion in one click — DocuGuru applies the official AIAA template with numbered references and exports a submission-ready PDF plus the editable LaTeX source. Free to start.
Jet propulsion is a peer-reviewed journal published by AIAA, covering Rocket and propulsion systems research, Diverse Scientific and Economic Studies, Human auditory perception and evaluation.
| Publisher | AIAA |
|---|---|
| Reference style | Numbered (AIAA) Numbered — [1], [2] in the text [1] Smith, A., Jones, B., and Lee, C., "A Representative Article Title," Jet propulsion, Vol. 12, No. 3, 2023, pp. 45–58.
Formats any DOI in Jet propulsion style. No sign-up. |
| Publishes research in | Rocket and propulsion systems research Diverse Scientific and Economic Studies Human auditory perception and evaluation Legal Cases and Commentary Legal case studies and regulations |
| ISSN | 0095-8751 |
| h-index | 35 |
| i10-index | 130 |
| Total citations | 6,846 |
| Top institutions publishing here | Princeton University |
| 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.
This paper deals wi th two l imit ing cases of laminar heat transfer over blunt-nosed bodies at hypersonic flight speeds, or high s tagnat ion temperatures: (a) thermodynamic equil ibrium, in which the chemical reaction rates are regarded as fas compared to the rates of diffusion across streamlines; (b) diffusion as rate-governing, in which…
Stagnation laminar heat transfer at hypersonic speeds depends on the rate of recombination of the dissociated air behind the detached shock wave. This paper is concerned with the case of a large recombination t ime compared to the t ime of diffusion across the boundary layer. The conditions of existence of such a frozen and…
A preliminary report of results obtained concerning radiation intensities measured with single Geiger tubes carried by Explorer I and III is presented. Resonable cosmic-ray counting rates were obtained for altitudes below about 1000 km. A plot of omnidirectional intensity vs. height in the vicinity of California for the first two weeks in February was obtained,…
The feasibility of a reaction device operating on intermittent gaseous detonation waves is considered. The results of a simplified theoretical analysis are presented and discussed. Preliminary experiments were conducted to determine the impulse derived from a single detonation wave and to investigate some of the more influential parameters: These tests were effected by suspending the…
