2014 IEEE Aerospace Conference 2014
DOI: 10.1109/aero.2014.6836242
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Designing a fuzzy logic controller for the Reynolds number in a blowdown supersonic wind tunnel

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Cited by 9 publications
(7 citation statements)
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“…Here, a 1 is a tting parameter, which can be expressed as a 1 475(κ 0 ) 2m 1 where κ 0 (2π/l 0 ) m 1 − 0.7 in which l 0 represents the inner scale of anisotropic turbulent plasma. e relation between L 0 and l 0 can be expressed as follows [26]:…”
Section: The Wave Structure Function Through Thementioning
confidence: 99%
“…Here, a 1 is a tting parameter, which can be expressed as a 1 475(κ 0 ) 2m 1 where κ 0 (2π/l 0 ) m 1 − 0.7 in which l 0 represents the inner scale of anisotropic turbulent plasma. e relation between L 0 and l 0 can be expressed as follows [26]:…”
Section: The Wave Structure Function Through Thementioning
confidence: 99%
“…where   (x, y) is the transverse spatial frequency, 2 Note that the relationship between L0 and l0 satisfies [46] 3/ 4 0…”
Section: Anisotropic Power Spectrum For Plasma Turbulencementioning
confidence: 99%
“…In the present study, the Reynolds number Re = 5 × 10 5 /m [20]. The Markov approximation is employed to obtain the anisotropic power spectra equation.…”
Section: Power Spectrum Of Refractive Index Fluctuation In Hypersonicmentioning
confidence: 99%