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- W1912004917 abstract "Abstract : Low density wind tunnel tests were carried out at Mach 2 and 3 to simulate the release of nitric oxide in the upper atmosphere from a sounding rocket. The supersonic flow contained atomic oxygen, and the wall-less chemiluminescent reaction of O with NO was investigated. Reaction rate constants thus obtained were up to 5 orders of magnitude higher than previously obtained laboratory rate constants." @default.
- W1912004917 created "2016-06-24" @default.
- W1912004917 creator A5042148844 @default.
- W1912004917 creator A5070339508 @default.
- W1912004917 date "1967-01-01" @default.
- W1912004917 modified "2023-09-26" @default.
- W1912004917 title "SIMULATION OF CHEMILUMINESCENT REACTION OF NITRIC OXIDE WITH ATOMIC OXYGEN IN A SUPERSONIC LOW DENSITY WIND TUNNEL, PART 2" @default.
- W1912004917 doi "https://doi.org/10.21236/ad0645516" @default.
- W1912004917 hasPublicationYear "1967" @default.
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