During the testing of a two-dimensional, streamlined aerodynamic shape, it is foundthat sonic conditions are first reached on the surface for a free-stream mach numberof 0.7. calculate the pressure coefficient at the point where this occurs, and also theminimum pressure coefficient for this shape in incompressible flow.

The temperature of air decreases as it is compressed by an adiabatic compressor. a)- true b)- false

During a steady flow process, the change of energy with respect to time is zero. a)- true b)- false

Afour cylinder four-stroke in-line engine has a stroke of 160mm, connecting rod length of 150mm, a reciprocating mass of 3kg and its firing order is 1-3-4-2. the spacing between cylinders is 100mm. i. show that the engine is in balance with regard to the primary inertia forces and primary 3. a and secondary inertia couples. li determine the out of balance secondary inertia force ii. propose ways of balancing this out of balance force and discuss the challenges that will arise