A subsonic diffuser flow is steady and adiabatic with inlet Mach number M1 = 0.6. Total pressure loss in the diffuser is 2% of the inlet total pressure, i. e., pt2/ pt1 = 0.98. The diffuser area ratio is A2/ A1 = 1.50. Assuming that the flow in the diffuser has a uniform exit flow, calculate the exit Mach number M2 the static pressure recovery in the diffuser CPR the (internal) force acting on the diffuser, i. e., Fx, wall, nondimensionalized by the inlet static pressure and ar

answer:

i dont know but you should start brainstorming ideas like how would you post them

explanation:

answer:

when he is talking to you he wont look at you or gaf that you are alive, that is how you know

explanation:

answer:

the formula for amps is watts divided by volts. to use the chart, cover up the a with your finger and use the remaining chart calculation of w divided by v. using our sample panel data, 60 watts divided by 12 volts equals 5 amps.

explanation:

answer:

in baseband transmission the whole bandwidth of the cable is utilized by a single signal. eg.Ethernet is using Basebands for LAN.

In the broadband transmission, multiple signals are sent on multiple frequencies simultaneously using a single channel. eg.Digital Subscriber Line (DSL)