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- W836771520 abstract "New turbojet-engine concept could reduce nitric oxide emissions to a level from one-fifteenth to as little as one three-hundredth that of conventional units. Multiple-stage combustor could overcome flame instability problems associated with previous low-flame-temperature systems. It operates in a relatively-simple adiabatic mode without elaborate fuel-flow and air circulation patterns.," @default.
- W836771520 created "2016-06-24" @default.
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- W836771520 date "1982-11-01" @default.
- W836771520 modified "2023-09-23" @default.
- W836771520 title "Staged Turbojet Engine Would Emit Less NO" @default.
- W836771520 hasPublicationYear "1982" @default.
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