Question

PYTHON CODE: Write a program that uses a while loop to examine every integer from 999...

PYTHON CODE:

Write a program that uses a while loop to examine every integer from 999 down to zero and generate the exact same output as shown blow. The range function is not required.

NOTE: you must use a while loop.

Required Output
960 920 880 840 800 760
720 680 640 600 560 520
480 440 400 360 320 280
240 200 160 120 80 40

0 0
Add a comment Improve this question Transcribed image text
Know the answer?
Add Answer to:
PYTHON CODE: Write a program that uses a while loop to examine every integer from 999...
Your Answer:

Post as a guest

Your Name:

What's your source?

Earn Coins

Coins can be redeemed for fabulous gifts.

Not the answer you're looking for? Ask your own homework help question. Our experts will answer your question WITHIN MINUTES for Free.
Similar Homework Help Questions
  • In C++ Programming: Using a single for loop, output the even numbers between 2 and 1004...

    In C++ Programming: Using a single for loop, output the even numbers between 2 and 1004 (inclusive) that iterates (loops) exactly 502 times. The outputted numbers be aligned in a table with 10 numbers per row. Each column in the table should be 5 characters wide. Do not nest a loop inside of another loop. Hint: First create and test the code that output the numbers all on one line (the command line will automatically wrap the output to new...

  • Can somone show me how to do the 1st problem? Need to find the LS and...

    Can somone show me how to do the 1st problem? Need to find the LS and SS for the fit and the LH and SH for the hole. Fits are all SHAFT BASIS METRIC but the shaft and hole diameters can not be used right out of the table. This is because the 3mm shaft tolerance does not match. You will need to lookup the "Fit" from the table, and then use the LS (Largest Shaft) and SS (Smallest Shaft)...

  • The Boeing 747 has a cruising altitude of 45,000 feet and cruising speed of 275 m/s....

    The Boeing 747 has a cruising altitude of 45,000 feet and cruising speed of 275 m/s. At this elevation, the temperature and pressure according to the US Standard Atmosphere (air properties as a function of altitude) are 220K and 1.8x104 Pa, respectively. The engines are steady state devices that can be modeled using the 1st Law of Thermodynamics with air (ideal gas) as the working fluid undergoing several processes. a. The inlet area of the engines is 0.5 m2. What...

  • We understand that your diagram will not be able to portray the bands to their exact base-pair si...

    We understand that your diagram will not be able to portray the bands to their exact base-pair size, and that in some cases you may not be able to calculate an exact size for your bands. Just do your best in terms of positioning the bands in the lanes with respect to the standard markers, but please do not panic if the bands are a couple of mm away from perfect in your diagram. LABEL each band with its size...

  • 174 2 combustor , =1500 K Problem 2 (22 pts): Brayton cycle and entropy calculations An...

    174 2 combustor , =1500 K Problem 2 (22 pts): Brayton cycle and entropy calculations An open Brayton cycle is used to generate electricity. Air enters the isentropic compressor at T1 = 300 K and P1 = 100 kPa with a mass flow rate m = 1.5 kg/s. The combustor can be modeled as a constant-pressure heat exchanger, supplying 1540 kW of thermal power to the air from a thermal reservoir (Th = 1750 K). Air enters the isentropic turbine...

  • 5) Evaluating Changes in Entropy for an Ideal Gas Air enters a turbine at 427 °C and 1 MPa and ex...

    5) Evaluating Changes in Entropy for an Ideal Gas Air enters a turbine at 427 °C and 1 MPa and exits at 127 °C. The outlet pressure can be tuned by the operator in the range from 300 - 800 kPa. Determine the change in specific entropy of the air, se -si, as it flows through this turbine 3 ways a) Assuming constant specific heats. b) Integrating an appropriate formula from Table A-2(c) from the text, which gives a polynomial...

  • Known Answer: W12=-51.0 Btu, constant Cv: Q12= -19.2 Btu, Table A-22E: Q12=-18.8 Btu....... Please explain in...

    Known Answer: W12=-51.0 Btu, constant Cv: Q12= -19.2 Btu, Table A-22E: Q12=-18.8 Btu....... Please explain in detail how to use the table. 3.145 Air is compressed in a piston-cylinder assembly from pi = 10 lbf/in?, T1 = 500°R to a final volume of K2 = 1 ft in a process described by pun = constant, where n= 1.25. The mass of air is 1/2 lbm. Assuming ideal gas behavior and neglecting kinetic and potential energy effects, determine the work and...

ADVERTISEMENT
Free Homework Help App
Download From Google Play
Scan Your Homework
to Get Instant Free Answers
Need Online Homework Help?
Ask a Question
Get Answers For Free
Most questions answered within 3 hours.
ADVERTISEMENT
ADVERTISEMENT
ADVERTISEMENT