Comment on “Jet propulsion by microwave air plasma in the atmosphere” [AIP Adv. 10, 055002 (2020)]
Source abstract
Abstract
In this Comment, we analyze the performance of a microwave plasma device presented by Ye et al. [AIP Adv. 10, 055002 (2020)]. The efficiency analysis, using conservation of energy, shows that the methods used by the original authors predict up to 8000% device efficiency. Our analytical model is based on a control volume analysis of the original authors’ experimental setup and conditions, indicating that blocking the exit of the device yields stagnation pressure rather than jet pressure. The results from this analysis are consistent with the reported experimental data, demonstrating that the measured pressure using this method is internal chamber pressure and cannot be used to estimate thrust.
Source: crossref · Quality: baseline
Research context
OpenAlex topics: Plasma and Flow Control in Aerodynamics · Plasma Diagnostics and Applications · Plasma Applications and Diagnostics
SciVX discovery tags are terminology-based. OpenAlex topics are source-provided classifications.
Affiliations
Mechanical and Aerospace Engineering Department, University of California , Los Angeles, California 90095, USA
Funding
National Aeronautics and Space Administration
References (10)
Show source-provided references
1. Jet propulsion by microwave air plasma in the atmosphere10.1063/5.0005814 ↗
2. 2008 · 27
3. 1992
4. Calculations of low-Reynolds-number resistojet nozzles10.2514/3.26431 ↗
5. Development and performance of the advanced radio frequency ion thruster RIT-XT
6. Development and testing of the Hayabusa2 ion engine system10.2322/tastj.14.pb_131 ↗
7. New low-power plasma thruster for nanosatellites
8. Maturation of iodine fueled BIT-3 RF ion thruster and RF neutralizer
9. Recent developments in DBD plasma flow control10.1016/j.paerosci.2013.05.003 ↗
10. First breakthrough for future air-breathing magneto-plasma propulsion systems10.1088/1742-6596/825/1/012005 ↗