1989
DOI: 10.2514/3.45768
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Surface-blowing anti-icing technique for aircraft surfaces

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Cited by 2 publications
(4 citation statements)
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“…Since there are many factors, the identification codes for each run were used as shown in Table 6. Tabrizi et al [13] used the slot and defined the ratio of maximum of velocity of injection from the hole to the maximum and minimum of wind tunnel speed and reported value of 22.16 and 3.6, respectively. In this study, this ratio is in the range of 3.8-5.7 for the separated holes.…”
Section: Resultsmentioning
confidence: 99%
See 1 more Smart Citation
“…Since there are many factors, the identification codes for each run were used as shown in Table 6. Tabrizi et al [13] used the slot and defined the ratio of maximum of velocity of injection from the hole to the maximum and minimum of wind tunnel speed and reported value of 22.16 and 3.6, respectively. In this study, this ratio is in the range of 3.8-5.7 for the separated holes.…”
Section: Resultsmentioning
confidence: 99%
“…They found that for any upstream and cylinder conditions, the location of slots could be optimum; therefore, the anti-icing system has its maximum effect. Tabrizi and Johanson [13] investigated experimentally to establish the effectiveness of surface blowing as an anti-icing for aircraft. They used circular cylinder with three span wise 4 by 0.014inch slots located at the frontal surface of the cylinder.…”
Section: Introductionmentioning
confidence: 99%
“…Tabrizi, et al [24] used slot injection with 0.004 in. by 4 in and the ratio of maximum of velocity of injection from the slot to the maximum and minimum of wind tunnel speed were reported 22.16 and 3.6, respectively.…”
Section: )mentioning
confidence: 99%
“…It was shown that for any upstream and cylinder conditions, the location of slots could be optimum, so that, the anti-icing system has its maximum effect. Further Tabrizi and Johanson [24] investigated experimentally to establish the effectiveness of surface blowing as an anti-icing for aircraft. A circular cylinder with three span wise 4 by 0.014 inch slots located at the frontal surface of the cylinder.…”
Section: Introductionmentioning
confidence: 99%