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Source of drage
Total Drag on an aerofoil is called profile drag
- Skin friction
• due to tangential force arising from friction
- Pressure
• Form - due to the integrated effect of pressuremodification from presence of the boundary layer
• Wave - due to the presence of shock waves
• The potential prediction of drag is zero- Inviscid, incompressible, irrotational
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DIVERGENT DUCT A divergent duct widens out as the airflow progresses through it. At subsonic speeds the effect of this kind of duct is to decrease the velocity and increase the p
Capital budgeting process: When investing in a long term assets, the project has been evaluated in term of its profitability and expected cash flow in the future. The capital budge
Flight dynmaics The study of aircraft- Stability & Trim (Equilibrium)- Motion due to • Control inputs • Atmospheric Disturbances • We will consider for the most part f
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Function intersect - set operations: The function intersect returns, additionally to the vector having the values in the intersection of v1 and v2, an index vector into v1 and
Limitations of shunt clippers
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