Question Set

1. Couple M is applied at C on a simply supported beam AB. What is the maximum shear force for the beam ?





Ask Your Doubts Here

Type in
(Press Ctrl+g to toggle between English and the chosen language)

Comments

Show Similar Question And Answers
QA->“Simply Fly”- ഏത് സ്ഥാപനത്തിന്റെ മുദ്രാവാക്യമാണിത്?....
QA->The internal force developed within a body when forces are applied on it is called?....
QA->Decrease of viscosity with increasing shear rate is known as....
QA->In a two roll mill the shear rate is adjusted by....
QA->The couple between base units of DNA is through which bonding?....
MCQ->Couple M is applied at C on a simply supported beam AB. What is the maximum shear force for the beam ? ....
MCQ->A fixed beam and a simply supported beam having same span and develop same maximum bending moment due to uniformly distributed load on entire span. What is the ratio of uniformly distributed load on fixed beam to that on simply supported beam ?....
MCQ->Consider the following statements regarding a simply supported beam subjected to a uniformly distributed load over the entire span : 1. The bending moment is maximum at the central position. 2. The shear force is zero at the central position. 3. The slope is maximum at the middle position. Of these statements :....
MCQ->The crane provides a long-reach capacity by using the telescopic boom segment DE. The entire boom is supported by a pin at A and by the telescopic hydraulic cylinder BC, which can be considered as a two-force member. The rated load capacity of the crane is measured by a maximum force developed in the hydraulic cylinder. If this maximum force is developed when the boom supports a mass m = 6 Mg and its length is l = 40 and = 60°, determine the greatest mass that can be supported when the boom length is extended to l = 50 m and = 45°. Neglect the weight of the boom and the size of the pulley at E. Assume the crane does not overturn. Note: when = 60° BC is vertical; however, when = 45° this is not the case.....
MCQ->Consider the following statements : 1. In a member subjected to uniaxial tensile force the maximum normal stress is the external load divided by the maximum cross-sectional area. 2. When the structural member is subjected to uniaxial loading, the shear stress is zero on a plane where the normal stress is maximum. 3. In a member subjected to uniaxial loading, the normal stress on the planes of maximum shear stress is less than the maximum. Of these statements :....
Terms And Service:We do not guarantee the accuracy of available data ..We Provide Information On Public Data.. Please consult an expert before using this data for commercial or personal use | Powered By:Omega Web Solutions
© 2002-2017 Omega Education PVT LTD...Privacy | Terms And Conditions
Question ANSWER With Solution