The pressure distribution of the naca0012 airfoil at zero angles of attack. airfoil equations can be found on the handout posted on blackboard or from online sources. compare its pressure distribution with the experimental data (find references) using a) 10, b) 20, and c) 100 panels equally distributed on both top and bottom side (that means twice the number of panels). comment on your results in the form of a report on

Afluid flows with a velocity field given by v=(x/t)i.. determine the local and convective accelerations when x=3 and t=1.

Consider a large isothermal enclosure that is maintained at a uniform temperature of 2000 k. calculate the emissive power of the radiation that emerges from a small aperture on the enclosure surface. what is the wavelength ? , below which 10% of the emission is concentrated? what is the wavelength ? 2 above which 10% of the emission is concentrated? determine the wavelength at which maximum spectral emissive power occurs. what is the irradiation incident on a small object placed inside the enclosure?

Prove the equivalence between the two statements of the 2nd law of thermodynamics (i.e., a violation of one statement leads to the violatio the other statement)