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A thin symmetric airfoil can deflect as slat and flap at positive (down) or negative (up) angles. The airfoil needs to produce a lift coefficient of c₁ = 0.6 without a suction peak and with neutral static stability. x = 0.15c α V∞ Tslat x= 0.8c Tflap a) Determine the angle of attack and the flap and slat deflection angles (assume small, state up/down) that meet the design requirements.

A thin symmetric airfoil can deflect as slat and flap at positive (down) or negative (up) angles. The airfoil needs to produce a lift coefficient of c₁ = 0.6 without a suction peak and with neutral static stability. x = 0.15c α V∞ Tslat x= 0.8c Tflap a) Determine the angle of attack and the flap and slat deflection angles (assume small, state up/down) that meet the design requirements.

Elements Of Electromagnetics
Elements Of Electromagnetics
7th Edition
ISBN:9780190698614
Author:Sadiku, Matthew N. O.
Publisher:Sadiku, Matthew N. O.
ChapterMA: Math Assessment
Section: Chapter Questions
Problem 1.1MA
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A thin symmetric airfoil can deflect as slat and flap at positive (down) or negative (up) angles. The airfoil needs to produce a lift coefficient of c₁ = 0.6 without a suction peak and with neutral static stability. x = 0.15c α V∞ Tslat x= 0.8c Tflap a) Determine the angle of attack and the flap and slat deflection angles (assume small, state up/down) that meet the design requirements.
Transcribed Image Text:A thin symmetric airfoil can deflect as slat and flap at positive (down) or negative (up) angles. The airfoil needs to produce a lift coefficient of c₁ = 0.6 without a suction peak and with neutral static stability. x = 0.15c α V∞ Tslat x= 0.8c Tflap a) Determine the angle of attack and the flap and slat deflection angles (assume small, state up/down) that meet the design requirements.
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