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Aeronautical Engineering
S/EN/46. Low Speed Aerodynamics: Pressure and Lift on Wing and Flap
- WORDS:
- 3100
- DATE:
- 2009
- PRICE:
- 39.99 GBP
The paper reports on the experiment conducted to measure pressure distribution on the wing consisting of a plain trailing edge flap. The changes in pressure distribution caused by the deflection of the flap are assessed considering integrated pressure across the chord giving lift co-efficient for varied combinations of angle of incidence and flap deflections. Flap effectiveness is calculated and compared to theoretical prediction.
KEYWORDS: Pressure distribution, wing, flap, lift co-efficient, angle of incidence, deflection,
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Keywords Tag Cloud
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