Abstract
This paper explores the use of Electromagnetic Radiation as an alternative to combustion in Scramjet-like hypersonic engines. The radiation is absorbed by the flow, heating it and thereby providing an alternative to the heat derived from combustion in the Scramjet. The advantages and disadvantages of this system are explored and theoretical results are presented illustrating typical radiation pathlengths at different frequencies. Suggestions for further theoretical and practical work are also made.
Original language | English |
---|---|
Pages (from-to) | 99-109 |
Number of pages | 11 |
Journal | JBIS - Journal of the British Interplanetary Society |
Volume | 62 |
Issue number | 3 |
Publication status | Published - Mar 2009 |
Keywords
- Electromagnetic activation
- Electromagnetic heating
- Scramjet