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TR8_ENGR111A_2011C (1)

Course: ENGR 111 A, Spring 2011
School: Texas A&M
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Info Time/Location: Exam Wed Oct 5 at 6:30pm 114 Richardson Multiple Choice and workout problems Alternative Exam (CVLB 421) 3:00pm and (CVLB 418) 4:30pm (Same Day) You arrange this with me by Monday Testable Topics (Problem Solving: Definition of Truss Stable Truss Force Components Cartesian Coord translation Moment (Torque) Cables/pulleys FBD Reaction/Resultant Forces Member Forces/Method of...

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Info Time/Location: Exam Wed Oct 5 at 6:30pm 114 Richardson Multiple Choice and workout problems Alternative Exam (CVLB 421) 3:00pm and (CVLB 418) 4:30pm (Same Day) You arrange this with me by Monday Testable Topics (Problem Solving: Definition of Truss Stable Truss Force Components Cartesian Coord translation Moment (Torque) Cables/pulleys FBD Reaction/Resultant Forces Member Forces/Method of Joints Zero Force Members by Inspection Factor of Safety ENGR 111 Track A 1 The Engineering Process: Using quantification to make decisions! Decision making from quantitative data: Will the truss withstand the necessary load? Calculation of the Safe Loads in a Truss TR-8 ENGR 111 Track A 2 Learning Objectives At the end of this module, you will be able to: Identify the two common modes of structural failure. Locate the links that are most likely to fail in a truss. Apply a standard procedure using the measured separation load on the links to calculate the allowable safe operating load on a truss. Apply Factor of Safety when necessary. ENGR 111 Track A 3 Safe Load on a Truss What is meant by the allowable design load on a truss? Allowable loads (working loads) are the forces to which the links can be safely subjected. This is the calculated load that can be applied to the truss which will just cause one of the links to fail. For the trusses (bridges) that you build, it is the load at which the link with the max tensile load separates from the magnet. ENGR 111 Track A 4 Quantification of Truss Failures How do we quantify collapse and deformation? The two principal modes of failure are (1) Failure by separation (tensile failure) (2) Failure by deflection (buckling) Failure by separation is quantified by the minimum load required to separate any portion of the truss from the rest. Failure by separation is caused by tensile loads. For the truss that we build, consider only tensile failure. Failure by deflection is quantified by the maximum amount of deflection that is allowed in any links of a truss even though it is not yet separated from the other links. Failure by deflection is caused by compressive loads. ENGR 111 Track A 5 Procedure for Identifying the Links at Risk How do we find the links in a truss that are at risk of failure? 1. Apply an external load of 1 lb or 1 N (or P) to the truss. 2. Find the internal forces in the links (numerical values or in terms of P). 3. Identify links that support largest loads. For our project, find the link(s) with the maximum tension (positive) loads. These are the links that are likely to fail in tension. ENGR 111 Track A 6 Calculating Safe Load on a Truss Max tensile load is the maximum load (force) that a tension member can support. Also, called tensile STRENGTH. Max allowable external load is the safe load on a truss. External Load La rgest Tensile Force = Max Allowable External Load Tensile STRENGTH ENGR 111 Track A 7 Example For the truss ABC 1. Find external reaction forces and axial forces in all truss members. 2. How much load can the truss carry if the max tensile load (strength) is 200 lb? Consider only tensile loads. ENGR 111 Track A 4 3 8 Example cont. 2. How much load can the truss carry if the max tensile load (strength) is 200 lb? Link Axial Force AB 1 lb (T) BC 1.33 lb (T) AC 1.67 lb (C) LinkBCsupportsthelargesttensileforce. LinkBCismorelikelytofailduetotension thanlinkAB. ENGR 111 Track A 9 Example cont. 2. How much load can the truss carry if the max tensile load (tensile strength) is 200 lb? P = 1 lb Internal force in BC = 1.33 lb External Load La rgest Tensile Force = Max Allowable External Load Tensile STRENGTH Pmax 200 lb 1 lb 1.33 lb = Pmax 200 lb Pmax = 150.4 lb ENGR 111 Track A 10 Example cont. If external load is given as P, then we calculate all internal forces in terms of P. Link P ( T) 7P 6 1. P (T) BC 1.33P (T) AC ) (C Axial Force AB 1.33P (T) 1.67P (C) LinkBCsupportsthelargesttensileforce. LinkBCismorelikelytofailduetotension thanlinkAB. ENGR 111 Track A 11 1.33P (T) 2. How much load can the truss carry if the max tensile load (tensile strength) is 200 lb? Bar BC supports the largest tensile force 1.33P. If we apply maximum allowable external load Pmax, bar BC will have to support 1.33Pmax. The max tensile load (tensile strength) that bar BC can support is 200 lb. If bar BC has to support more than 200 lb it will fail. ENGR 111 Track A P ( T) Example cont. 7P 6 1. C) ( 1.33Pmax = 200 lb Pmax = 150.4 lb 12 Load Scaling Link Force Axial Look at the internal forces calculated in terms of P: AB P (T) BC 1.33P (T) AC 1.67P (C) Load in the bars (axial force) is scaled with the applied external Load! Why? All the equations of equilibrium were linear equations for the forces! ENGR 111 Track A 13 Factor of Safety In project 1, we need to design a bridge that should be able to carry a test load of at least 2 lb applied at (or near) the center of top of the span. We probably would like to make our bridges a little bit stronger than that. Engineers account for various uncertainties by making structures stronger than they really need to be. How? They use a Factor of Safety in all analysis and design calculations. Failure Level Factor of Safety = Actual Level ENGR 111 Track A 14 Factor of Safety for a Truss A truss is only as strong as its weakest link. For a truss, we can define the factor of safety as Failure Level Strength Factor of Safety = = Actual Level Internal Member Force P (T) 1.33P (T) P 67 1. ) (C Example: External load P = 100 lb. Tensile strength of the bars is 200 lb. Compressive strength of the bars is 180 kN. FSAB = 200 lb / 100 lb = 2 FSBC = 200 lb / 133 lb = 1.5 FSAC = 180 lb / 167 lb = 1.08 Factor of Safety for the truss is 1.08 (the most conservative value) ENGR 111 Track A 15 Example: for the truss below, internal forces in all truss members have been calculated. Consider both modes of failure and Determine factor of safety for the truss. 11.9kN 15kN 12kN 11.9kN 0.86kN 0.71kN 12kN 0.71kN 12kN ENGR 111 Track A 15kN 12kN 16 AB, FH 15 kN (C) Given: The tensile strength of the bars is 50 kN. The compressive strength of the bars is 45 kN. BD, DF 11.9 kN (C) Determine factor of safety for the truss. BE, EF 0.71 kN (C) Factor of Safety = AC, CE, EG, GH 12 kN (T) DE 0.86 kN (T) Member BC, FG Force zero Strength Internal Member Force The largest tensile force in the links is 12 kN. FS = 50 kN / 12 kN = 4.17 The largest compressive force in the links is 15 kN. FS = 45 kN / 15 kN = 3 Links AB and FH have the smallest factor of safety (compressive and tensile loads). If AB and/or FH fail, the whole structure collapses. Hence, the Factor of Safety for the truss is 3 we pick the most conservative value. ENGR 111 Track A 17 Exercise 1 - Individual The max allowable tensile load for the links in the truss shown is 75 N and the max allowable compressive load for the links is 90 N. Find the max allowable value of P. Determine the factor of safety for the structure if P = 100 N. B D 60 A 1m 60 C 2m P/2 E 1m H P/2 ENGR 111 Track A 18 What if your truss is subjected to several external forces? Example 1. For the truss shown, lets assume we found that the largest tensile force in the links is 3 kN. The tensile strength is 4 kN. How do we calculate the max allowable load for the truss? Total external load applied is 5 kN. 3 kN 2 kN Make a proportion. External load / Pmax = Largest Internal Force / STRENGTH 5 kN / Pmax = 3 kN / 4 kN Solve for Pmax. ENGR 111 Track A 19 What if your truss is subjected to several external forces? Example 2. For the truss shown, we found that all blue links are in tension and all grey links are in compression. Internal force in each blue link is different: P T1 =0.55P, T2 = 1.2P, T3 = 0.8P The largest tensile force is T2 = 1.2P 1.5P How do we calculate the max allowable load for the truss T1 T2 T3 if we have to consider only tensile loads? Total external load applied is P + 1.5P = 2.5P = Ptotal Make a proportion: Ptotal / Ptotalmax = 1.2P / STRENGTH 2.5P / Ptotalmax = 1.2P / STRENGTH If tensile STRENGTH is given, you can calculate P totalmax. ENGR 111 Track A 20 What if your truss is subjected to several external forces? Example 3. How do we calculate the max allowable load for the truss if we have to consider all loads (tensile and compressive)? Lets assume that we found that maximum tensile force in a truss member is T = 1.2P and maximum compressive force in a truss member is C = 1.5P. P Given: max tensile STRENGTH is 500 lb max compressive STRENGTH is 300 lb 1.5P Total external load applied is P + 1.5P = 2.5P = Ptotal Make a proportion: 2.5P / Ptotalmax = Largest Internal Force / STRENGTH For the tensile member: 2.5*P / Ptotalmax = 1.2*P / 500 lb Ptotalmax = 833.4 lb For the compressive member: 2.5*P / Ptotalmax = 1.5*P / 300 lb Ptotalmax = 500 lb Pick the most conservative value for the max allowable load on the truss: Ptotalmax = 500 lb. ENGR 111 Track A 21
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University of Texas - M - 346
University of Texas - M - 346
University of Texas - M - 346
University of Texas - M - 346
University of Texas - M - 346
University of Texas - M - 346
University of Texas - M - 346
University of Texas - M - 346
University of Texas - M - 346
University of Texas - M - 346
University of Texas - M - 346
University of Texas - M - 346