47th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition 2009
DOI: 10.2514/6.2009-779
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Numerical Study on Flow Control by Micro-Blowing

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Cited by 18 publications
(7 citation statements)
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“…Kornilov / Progress in Aerospace Sciences ∎ (∎∎∎∎) ∎∎∎-∎∎∎ blowing intensity rises [94]. The perforated wall with staggered orifices turned out to be more effective than the similar wall with tandem orifices.…”
Section: Characteristics Of the Modified Flowmentioning
confidence: 97%
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“…Kornilov / Progress in Aerospace Sciences ∎ (∎∎∎∎) ∎∎∎-∎∎∎ blowing intensity rises [94]. The perforated wall with staggered orifices turned out to be more effective than the similar wall with tandem orifices.…”
Section: Characteristics Of the Modified Flowmentioning
confidence: 97%
“…Note that using a numerical calculation for М 1 ¼ 0.7 and blowing coefficient equal to 0.015, the total drag reduction of about 3.2% was obtained in [94].…”
Section: Total Drag Reductionmentioning
confidence: 98%
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“…Stanewksy [8] extensively studied various conventional means of flow control in case of moderate to large aspect ratio wings, delta wings. Li et al [9] proposed micro-blowing as another flow control technique. However, these active flow control methods are not always economically viable.…”
Section: Introductionmentioning
confidence: 99%