2nd AIAA "Unmanned Unlimited" Conf. And Workshop &Amp; Exhibit 2003
DOI: 10.2514/6.2003-6528
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A Mission Based Optimization Study of Engine Configurations for a Low-Signature Reconaissance UAV - A Multi-Objective Approach

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“…Trends in thermodynamic cycle parameters which improve the cycle efficiency and lower fuel consumption also lower the heat rejection from engine. Therefore, for given operating point, these trends also lower engine IRSLs [67,110]; however, afterburning increases IR emissions by almost 10-folds [67]. A non-axisymmetric nozzle has lesser IR emissions than an axisymmetric nozzle, because the internal engine hot parts are largely masked by the non-axisymmetric nozzle hardware [102].…”
Section: Exhaust Systemmentioning
confidence: 95%
“…Trends in thermodynamic cycle parameters which improve the cycle efficiency and lower fuel consumption also lower the heat rejection from engine. Therefore, for given operating point, these trends also lower engine IRSLs [67,110]; however, afterburning increases IR emissions by almost 10-folds [67]. A non-axisymmetric nozzle has lesser IR emissions than an axisymmetric nozzle, because the internal engine hot parts are largely masked by the non-axisymmetric nozzle hardware [102].…”
Section: Exhaust Systemmentioning
confidence: 95%