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please solve this thanks the answear is IPN380 3-16 A simple beam with an overhang is subjected to a point load P...
post only Group#7 Problem 5 (6 marks) For the beam and loading shown, a) Draw the...
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only Group#7
Problem 5 (6 marks) For the beam and loading shown, a) Draw the shear and bending-moment diagrams. b) Determine the maximum absolute value of the shear and bending moment. c) Determine the minimum required depth h of the beam. Knowing that the material used has an ultimate normal and shear stresses, use the given factor of safety in each loading case in the following table. P A LLL Dimensions, material properties and load values are presented in...
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)...
40kN Uniform Load W kN/m X Span L L/2 Figure 1 SPAN L 6 W 11Kn/m Beam is 200 UB 18.2 Use the diagram above and the W an...
40kN Uniform Load W kN/m X Span L L/2 Figure 1 SPAN L 6 W 11Kn/m Beam is 200 UB 18.2 Use the diagram above and the W and L values assigned to you to: a) Use your shear force diagram to calculate the Maximum longitudinal Shear Stress and where it occ Ccurs. b) Calculate the longitudinal Shear Stress at d/4 from the neutral axis. Check Figures 283 below this table BENDING MOMENT DIAGLAM Kp/m f:40 zm 7.5 KN-M 90...
Problem (42-43) 50 ksi steel, by Calculation: Select the lightest w section for a beam 20...
Problem (42-43) 50 ksi steel, by Calculation: Select the lightest w section for a beam 20 ft in length with a superimposed total uniformly distributed live load of 98 kips and a total uniformly distributed dead load of 50 kips. DO NOT adjust for beam self weight Question 42 Not yet answered Points out of 3.00 P Flag question Lightest W- Select one O a, W24x62 Ob W18x71 O C. W24x55 O d. w12x79 Question 43 Flag question Not yet...
CRBEMENo 6 (16 points) Answer the following questions about rolled steel W-beams (use the sable provided...
CRBEMENo 6 (16 points) Answer the following questions about rolled steel W-beams (use the sable provided as necessary): Which one of the following characteristics makes a W-beam "optimal" (as i. assumed for this class)? a narrowest flange width largest section modulus lightest weight shallowest depth d. Ir the beam is bent about horizontal x-x avis and requires a minimum section modulus of 43.4 in', which of the following beams would make the "short list"? (For this question only, mark all...
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...
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...
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...
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...
post
only Group#7
Problem 5 (6 marks) For the beam and loading shown, a) Draw the shear and bending-moment diagrams. b) Determine the maximum absolute value of the shear and bending moment. c) Determine the minimum required depth h of the beam. Knowing that the material used has an ultimate normal and shear stresses, use the given factor of safety in each loading case in the following table. P A LLL Dimensions, material properties and load values are presented in...
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)...
40kN Uniform Load W kN/m X Span L L/2 Figure 1 SPAN L 6 W 11Kn/m Beam is 200 UB 18.2 Use the diagram above and the W and L values assigned to you to: a) Use your shear force diagram to calculate the Maximum longitudinal Shear Stress and where it occ Ccurs. b) Calculate the longitudinal Shear Stress at d/4 from the neutral axis. Check Figures 283 below this table BENDING MOMENT DIAGLAM Kp/m f:40 zm 7.5 KN-M 90...
Problem (42-43) 50 ksi steel, by Calculation: Select the lightest w section for a beam 20 ft in length with a superimposed total uniformly distributed live load of 98 kips and a total uniformly distributed dead load of 50 kips. DO NOT adjust for beam self weight Question 42 Not yet answered Points out of 3.00 P Flag question Lightest W- Select one O a, W24x62 Ob W18x71 O C. W24x55 O d. w12x79 Question 43 Flag question Not yet...
CRBEMENo 6 (16 points) Answer the following questions about rolled steel W-beams (use the sable provided as necessary): Which one of the following characteristics makes a W-beam "optimal" (as i. assumed for this class)? a narrowest flange width largest section modulus lightest weight shallowest depth d. Ir the beam is bent about horizontal x-x avis and requires a minimum section modulus of 43.4 in', which of the following beams would make the "short list"? (For this question only, mark all...
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...
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...
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...
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