aee 716 aircraft icing - metuae716/lecture-5web.pdf · 2011. 4. 26. · ttw search in utim using...
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AEE 716 Aircraft Icing
Prof. Dr. Serkan ÖZGENDept. Aerospace Engineering, METU
Spring 2010-2011
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Outline
• Three dimensional panel method• Droplet trajectories and collection efficiencies• Calculation of convective heat transfer coefficients• Extended Messinger Model• Validation results• Wing geometry results• Intake geometry results
Serkan ÖZGEN 2
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Flow chart of the method
Serkan ÖZGEN 3
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Particle trajectories
Serkan ÖZGEN 4
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Droplet impact determination
Serkan ÖZGEN 5
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Droplet collection efficiency determination
Serkan ÖZGEN 6
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Droplet collection efficiency distribution
Serkan ÖZGEN 7
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Validation results
Serkan ÖZGEN 8
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Validation results
Serkan ÖZGEN 9
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Validation results
Serkan ÖZGEN 10
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Validation results
Serkan ÖZGEN 11
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Validation results
Serkan ÖZGEN 12
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Circular Intake
Serkan ÖZGEN 13
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Circular Intake
Serkan ÖZGEN 14
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Circular Intake
Serkan ÖZGEN 15
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Circular Intake
Serkan ÖZGEN 16
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Circular Intake
Serkan ÖZGEN 17
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Validation results
Serkan ÖZGEN 18
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Elliptical Intake
Serkan ÖZGEN 19
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Elliptical Intake
Serkan ÖZGEN 20
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Elliptical Intake
Serkan ÖZGEN 21
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Elliptical Intake
Serkan ÖZGEN 22
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Validation results
Serkan ÖZGEN 23
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Turboprop Intake
Serkan ÖZGEN 24
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Turboprop Intake
Serkan ÖZGEN 25
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Turboprop Intake
Serkan ÖZGEN 26
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Turboprop Intake
Serkan ÖZGEN 27
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Turboprop Intake
Serkan ÖZGEN 28
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Turboprop Intake
Serkan ÖZGEN 29