What are the final values of them after the execution of the program?

The following is an assembly program.

 

CODE SEGMENT

START: MOV AX, DATA

MOV DS, AX

MOV CX, 3

MOV SI, OFFSET ARRAY

ITER: MOV AX, [SI]

XCHG AH, AL

ROL AX, 1

INC SI

AND [SI], AX

LOOP ITER

ENDS

 

DATA SEGMENT

DB 6 DUP (0)

ARRAY DB 0B9H,8BH,01H,70H,02H,06H,34H,0CH

ENDS

 

END START

 

Enter the above program in emu8086, obtain the list file and single step the program, to complete tasks and answer questions below.

 

  1. Fill in the blanks in the following table after each instruction is executed for the first run of the ITER loop:
Run 1 AX CX SI 8-bit data in DS:SI 8-bit data in DS:SI+1
MOV AX, [SI]          
XCHG AH, AL          
ROL AX, 1          
INC SI          
AND [SI], AX          
LOOP ITER          

 

The data of the 8 memory locations starting from ARRAY at the end of Run 1:

               

 

What is the function of ROL? Use the numbers in ROL AX,1 to explain.

What is the function of AND?

  1. Fill in the blanks in the following table after each instruction is executed for the second run of the ITER loop:

 

Run 2 AX CX SI 8-bit data in DS:SI 8-bit data in DS:SI+1
MOV AX, [SI]          
XCHG AH, AL          
ROL AX, 1          
INC SI          
AND [SI], AX          
LOOP ITER          

 

The data of the 8 memory locations starting from ARRAY at the end of Run 2:

               

 

What are the final values of them after the execution of the program? Explanation and screenshot are required.

  1. If the data transferred into CX is 6, how many times will the LOOP instruction execute?

Write an equivalent instruction to MOV AX,DATA using array.

find the cost of your paper

Determine the thrust available to propel the cart.

A CO2 cartridge is used to propel a small rocket cart. Compressed gas, stored at 35 MPa and 20C, is expanded through a smoothly contoured converging nozzle with 0.5 mm….

Determine the range(s) of inlet stagnation pressures for which the nozzle will be free from normal shocks.

A converging-diverging nozzle, with Ae/At 5 1.633, is designed to operate with atmospheric pressure at the exit plane. Determine the range(s) of inlet stagnation pressures for which the nozzle will….

Find the range of exit pressures for which the duct exit flow is choked.

Room air is drawn into an insulated duct of constant area through a smoothly contoured converging nozzle. Room conditions are T 5 80 F and p 5 14:7 psia. The….