Aircraft Systems and Technology Meeting 1979
DOI: 10.2514/6.1979-1813
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Nozzle design and integration in an advanced supersonic fighter

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“…The IRSS system consists of any of the following or a combination of the following four techniques/ components: (i) Masking of hot engine parts; which includes nozzle shape alteration [101][102][103][104], jet pipe geometry modification [3,105], and fitment of new assembly [106,107]. (ii) Peak temperature reduction of exhaust gases by enhancing mixing with the surroundings.…”
Section: Passive Countermeasuresmentioning
confidence: 99%
“…The IRSS system consists of any of the following or a combination of the following four techniques/ components: (i) Masking of hot engine parts; which includes nozzle shape alteration [101][102][103][104], jet pipe geometry modification [3,105], and fitment of new assembly [106,107]. (ii) Peak temperature reduction of exhaust gases by enhancing mixing with the surroundings.…”
Section: Passive Countermeasuresmentioning
confidence: 99%