The literature contains many theoretical analyses describing combustion instability of solid propellants. The majority of these have been applied Io acoustic instability and are therefore framed in a format compatible with the acoust,cs of a rocket chamber. Howuver. in the low frequency r6gim¢ these
NMR properties of N3−. A comparison of theory and experiment
✍ Scribed by Michał Jaszuński; Sławomir Szymański; Ove Christiansen; Poul Jørgensen; Trygve Helgaker; Kenneth Ruud
- Publisher
- Elsevier Science
- Year
- 1995
- Tongue
- English
- Weight
- 539 KB
- Volume
- 243
- Category
- Article
- ISSN
- 0009-2614
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