1 Why influence lines?1 Mengapa influence line?
Key pointsIsi penting
- An influence line gives one response at a fixed point as a unit load moves.
- It is not a shear-force or bending-moment diagram: there the loads are fixed and the section moves.
- Superposition makes it reusable for any pattern of loads.
- Influence line memberi satu response pada titik tetap semasa unit load bergerak.
- Ia bukan shear-force atau bending-moment diagram: dalam diagram itu load tetap dan section yang berubah.
- Superposition membolehkan ia digunakan semula untuk sebarang susunan load.
Most structures are designed for loads that stay where they are: the weight of a floor, the water in a tank. A bridge, a crane girder or a gantry rail carries loads that move, and the designer must answer a question that a shear-force diagram cannot: where must the vehicle stand to produce the largest reaction at a pier, the largest shear at a section, or the largest moment at midspan? The influence line answers it directly.
Kebanyakan struktur direka untuk load yang kekal di tempatnya: berat lantai, air dalam tangki. Jambatan, crane girder atau gantry rail pula membawa load yang bergerak, dan pereka perlu menjawab soalan yang tidak dapat dijawab oleh shear-force diagram: di mana kenderaan perlu berada untuk menghasilkan reaction terbesar pada pier, shear terbesar pada sesuatu section, atau moment terbesar di midspan? Influence line menjawabnya secara terus.
| Shear-force / bending-moment diagram | Influence line | |
|---|---|---|
| What is fixedApa yang tetap | the loadsload | the point where \(R\) is evaluatedtitik di mana \(R\) dinilai |
| What varies along the abscissaApa yang berubah pada paksi-x | the section where \(V\) or \(M\) is readsection di mana \(V\) atau \(M\) dibaca | the position \(x\) of the unit loadkedudukan \(x\) unit load |
| What the ordinate meansMaksud ordinate | \(V\) or \(M\) at that section, for the given loads\(V\) atau \(M\) pada section itu, untuk load yang diberi | \(R\) at the fixed point, for a unit load standing at \(x\)\(R\) pada titik tetap, untuk unit load di \(x\) |
For a linear elastic structure the response is proportional to the load and the effects of several loads add (superposition). That is what makes the influence line useful: once \(\eta_R(x)\) is known for a unit load, the effect of any pattern of concentrated or distributed loads follows by multiplication and addition (Section 5).
Bagi struktur linear elastic, response berkadar dengan load dan kesan beberapa load boleh dijumlahkan (superposition). Inilah yang menjadikan influence line berguna: sebaik sahaja \(\eta_R(x)\) diketahui untuk unit load, kesan sebarang susunan concentrated load atau distributed load diperoleh melalui pendaraban dan penambahan (Section 5).
On the influence line for \(R_A\), the horizontal axis is …Pada influence line bagi \(R_A\), paksi mendatar ialah …
\(R_A\) is always read at A; what changes is where the unit load stands.\(R_A\) sentiasa dibaca di A; yang berubah ialah kedudukan unit load.
2 The laboratory model2 Model makmal
Key pointsIsi penting
- ABC and DEF: beams on two supports with a 190 mm cantilever; CD: suspended span on hinges C and D.
- Pins (A, F) and rollers (B, E) are supports; hinges (C, D) are joints that pass force but no moment.
- 4 unknown reactions, 2 equilibrium equations + 2 hinge conditions: statically determinate.
- So every influence line is straight-segmented, kinked only at hinges.
- Reactions positive upwards; \(R_C\), \(R_D\) positive pressing down on the tips.
- ABC dan DEF: beam atas dua support dengan cantilever 190 mm; CD: suspended span pada hinge C dan D.
- Pin (A, F) dan roller (B, E) ialah support; hinge (C, D) ialah sambungan yang memindahkan daya tetapi tidak memindahkan moment.
- 4 reaction yang tidak diketahui, 2 persamaan equilibrium + 2 syarat hinge: statically determinate.
- Maka setiap influence line terdiri daripada segmen lurus, berbengkok hanya di hinge.
- Reaction positif ke atas; \(R_C\), \(R_D\) positif apabila menekan ke bawah pada hujung cantilever.
The model is a cantilever bridge of the type patented by Heinrich Gerber in 1866 and used, at a very different scale, in the Forth Bridge: two anchor spans with cantilever arms, and a suspended span that rests on the tips of the arms through hinges.
Model ini ialah cantilever bridge jenis yang dipatenkan oleh Heinrich Gerber pada 1866 dan digunakan, pada skala yang jauh berbeza, pada Forth Bridge: dua anchor span dengan cantilever arm, dan suspended span yang terletak di hujung arm melalui hinge.
Members. Beam ABC is simply supported at A and B with a cantilever BC of 190 mm. Beam DEF is its mirror image. The suspended span CD (250 mm) rests on the cantilever tips: the hinges transmit a vertical force but no bending moment.
Anggota. Beam ABC disokong mudah di A dan B dengan cantilever BC sepanjang 190 mm. Beam DEF ialah imej cerminnya. Suspended span CD (250 mm) terletak di hujung cantilever: hinge memindahkan daya menegak tetapi tidak memindahkan bending moment.
Supports and hingesSupport dan hinge
A support or a joint is described by what it stops: every movement it prevents produces a force (or moment) in that direction, and every movement it allows produces none.
Sesuatu support atau sambungan diterangkan berdasarkan apa yang ia halang: setiap pergerakan yang dihalang menghasilkan daya (atau moment) pada arah itu, dan setiap pergerakan yang dibenarkan tidak menghasilkan apa-apa.
| Restraint | WhereLokasi | TransmitsMemindahkan | AllowsMembenarkan |
|---|---|---|---|
| Pin | A, F | vertical and horizontal forcedaya menegak dan mendatar | rotationputaran |
| Roller | B, E | vertical force onlydaya menegak sahaja | rotation and horizontal movementputaran dan pergerakan mendatar |
| Hinge (internal)Hinge (dalaman) | C, D | force between the two members it joinsdaya antara dua anggota yang disambung | relative rotation, so \(M = 0\) at the hingeputaran relatif, maka \(M = 0\) di hinge |
Because a hinge carries no moment, each hinge adds one equation, \(M = 0\) at that point, and this is what makes the model statically determinate (next paragraph). In the model the supports at A and F can also pull downwards: the gauges there register uplift as a negative reading.
Oleh kerana hinge tidak membawa moment, setiap hinge menambah satu persamaan, \(M = 0\) pada titik itu, dan inilah yang menjadikan model ini statically determinate (perenggan seterusnya). Dalam model ini, support di A dan F juga boleh menarik ke bawah: gauge di situ merekodkan uplift sebagai bacaan negatif.
At which point can the model carry a bending moment?Pada titik manakah model ini boleh membawa bending moment?
Beam ABC is continuous over B, so it carries moment there (that is why it can cantilever out to C). The hinge at C lets the two members rotate relative to each other, so the moment there is zero.Beam ABC selanjar melalui B, jadi ia membawa moment di situ (sebab itulah ia boleh menjulur sebagai cantilever hingga C). Hinge di C membenarkan dua anggota berputar relatif antara satu sama lain, jadi moment di situ sifar.
Determinacy. No horizontal load is applied, so there are four unknown vertical reactions \(R_A, R_B, R_E, R_F\). Statics gives two useful equations for the whole structure (\(\sum F_y = 0\), \(\sum M = 0\)) and each internal hinge one more (\(M = 0\) at C and at D): four equations for four unknowns. The structure is statically determinate, every influence line follows from equilibrium alone with no need for \(EI\), and every influence line is made of straight segments.
Determinacy. Tiada load mendatar dikenakan, jadi terdapat empat reaction menegak yang tidak diketahui, \(R_A, R_B, R_E, R_F\). Statik memberi dua persamaan berguna bagi keseluruhan struktur (\(\sum F_y = 0\), \(\sum M = 0\)) dan setiap hinge dalaman memberi satu lagi (\(M = 0\) di C dan di D): empat persamaan untuk empat anu. Struktur ini statically determinate; setiap influence line diperoleh daripada equilibrium sahaja tanpa memerlukan \(EI\), dan setiap influence line terdiri daripada segmen lurus.
Sign convention. Support reactions are positive upwards. The hinge forces \(R_C\) and \(R_D\) are the forces the suspended span presses on the cantilever tips (positive downwards on the tip); they are what the gauges at C and D register. Positions are measured from A, \(0 \le x \le 1130\) mm.
Sign convention. Support reaction positif ke atas. Hinge force \(R_C\) dan \(R_D\) ialah daya yang dikenakan oleh suspended span ke atas hujung cantilever (positif ke bawah pada hujung); inilah yang direkod oleh gauge di C dan D. Kedudukan diukur dari A, \(0 \le x \le 1130\) mm.
3 Deriving the influence lines3 Menerbitkan influence line
Key pointsIsi penting
- Analyse the suspended span first; take moments about a support every time.
- On ABC: \(\eta_A = (250-x)/250\), \(\eta_B = x/250\); at the tip C: −0.76 and 1.76.
- On CD: \(\eta_C = (690-x)/250\), \(\eta_D = (x-440)/250\); then \(\eta_A = -0.76\,\eta_C\), \(\eta_B = 1.76\,\eta_C\).
- \(\eta_C\), \(\eta_D\) are non-zero only for a load on CD: only then does the suspended span pass force through the hinges.
- Check: \(\eta_A+\eta_B+\eta_E+\eta_F = 1\) at every \(x\).
- Analisis suspended span dahulu; ambil moment terhadap support setiap kali.
- Pada ABC: \(\eta_A = (250-x)/250\), \(\eta_B = x/250\); di hujung C: −0.76 dan 1.76.
- Pada CD: \(\eta_C = (690-x)/250\), \(\eta_D = (x-440)/250\); kemudian \(\eta_A = -0.76\,\eta_C\), \(\eta_B = 1.76\,\eta_C\).
- \(\eta_C\), \(\eta_D\) bukan sifar hanya bagi load pada CD: hanya ketika itu suspended span memindahkan daya melalui hinge.
- Semakan: \(\eta_A+\eta_B+\eta_E+\eta_F = 1\) bagi setiap \(x\).
The derivation uses one idea three times: take moments about a support. The order matters: the suspended span is analysed first, because it is the only member whose loads reach the others.
Derivation ini menggunakan satu idea sebanyak tiga kali: ambil moment terhadap support. Urutan penting: suspended span dianalisis dahulu, kerana hanya anggota ini yang load-nya sampai kepada anggota lain.
Step 1 · Unit load on beam ABCLangkah 1 · Unit load pada beam ABC \((0 \le x \le 440)\)
Isolate ABC (panel a). It carries the unit load at \(x\) and the reactions \(R_A\), \(R_B\); the hinge at C is unloaded because the suspended span carries nothing. Moments about B:Asingkan ABC (panel a). Ia membawa unit load di \(x\) serta reaction \(R_A\), \(R_B\); hinge di C tidak dibebani kerana suspended span tidak membawa apa-apa. Moment terhadap B:
\[ R_A\cdot 250 - 1\cdot(250-x) = 0 \;\Longrightarrow\; \eta_A(x) = \frac{250-x}{250},\qquad \eta_B(x) = 1-\eta_A(x) = \frac{x}{250}. \]Nothing in this result stops at \(x = 250\): for a load on the cantilever the lever arm \((250 - x)\) is negative, so \(\eta_A\) is negative (support A must hold the beam down) and \(\eta_B\) exceeds 1. At the tip, \(\eta_A(440) = -190/250 = -0.76\) and \(\eta_B(440) = 440/250 = 1.76\).Tiada apa dalam keputusan ini yang berhenti di \(x = 250\): bagi load pada cantilever, lever arm \((250 - x)\) adalah negatif, maka \(\eta_A\) negatif (support A perlu menahan beam ke bawah) dan \(\eta_B\) melebihi 1. Di hujung, \(\eta_A(440) = -190/250 = -0.76\) dan \(\eta_B(440) = 440/250 = 1.76\).
Step 2 · Unit load on the suspended span CDLangkah 2 · Unit load pada suspended span CD \((440 \le x \le 690)\)
CD is a simply supported beam of span 250 mm resting on the hinges (panel b), so the hinge forces follow the lever rule:CD ialah simply supported beam dengan span 250 mm yang terletak pada hinge (panel b), jadi hinge force mengikut lever rule:
\[ \eta_C(x) = \frac{690-x}{250},\qquad \eta_D(x) = \frac{x-440}{250},\qquad \eta_C+\eta_D = 1. \]Step 3 · Carry the hinge force into beam ABCLangkah 3 · Pindahkan hinge force ke beam ABC
With the load on CD, beam ABC carries only the downward force \(\eta_C\) at its tip (panel c). This is Step 1 with the load \(\eta_C\) standing at \(x = 440\):Apabila load berada pada CD, beam ABC hanya membawa daya ke bawah \(\eta_C\) di hujungnya (panel c). Ini sama seperti Langkah 1 dengan load \(\eta_C\) di \(x = 440\):
\[ \eta_A(x) = \eta_C(x)\,\frac{250-440}{250} = -0.76\,\eta_C(x),\qquad \eta_B(x) = \eta_C(x)\,\frac{440}{250} = 1.76\,\eta_C(x). \]At C both expressions for \(\eta_A\) give \(-0.76\), so the line is continuous; at D, \(\eta_C = 0\) and therefore \(\eta_A = \eta_B = 0\).Di C kedua-dua ungkapan bagi \(\eta_A\) memberi \(-0.76\), jadi garisnya selanjar; di D, \(\eta_C = 0\) dan oleh itu \(\eta_A = \eta_B = 0\).
Step 4 · Unit load on beam DEFLangkah 4 · Unit load pada beam DEF \((690 \le x \le 1130)\)
DEF is the mirror image of ABC about the centre of the model (\(x = 565\) mm), with E playing the part of B and F that of A:DEF ialah imej cermin ABC terhadap tengah model (\(x = 565\) mm), dengan E mengambil peranan B dan F peranan A:
\[ \eta_F(x) = \frac{x-880}{250},\qquad \eta_E(x) = \frac{1130-x}{250}. \]For a load on CD the hinge force \(\eta_D\) is carried by DEF exactly as \(\eta_C\) was by ABC: \(\eta_E = 1.76\,\eta_D\), \(\eta_F = -0.76\,\eta_D\). A load on ABC never reaches DEF, and vice versa, because the suspended span is then unloaded and transmits nothing.Bagi load pada CD, hinge force \(\eta_D\) dibawa oleh DEF sama seperti \(\eta_C\) dibawa oleh ABC: \(\eta_E = 1.76\,\eta_D\), \(\eta_F = -0.76\,\eta_D\). Load pada ABC tidak pernah sampai ke DEF, dan sebaliknya, kerana suspended span ketika itu tidak dibebani dan tidak memindahkan apa-apa.
Why ηC and ηD are non-zero only between C and DMengapa ηC dan ηD bukan sifar hanya antara C dan D
The gauge at C reads the force that passes through hinge C, from the suspended span into the tip of cantilever BC. A force can pass through the hinge only when the suspended span itself carries something.Gauge di C membaca daya yang melalui hinge C, dari suspended span ke hujung cantilever BC. Daya hanya boleh melalui hinge apabila suspended span itu sendiri membawa sesuatu.
- Load on ABC (\(x \lt 440\)): ABC stands on its own supports A and B and takes the load to them directly. The suspended span carries nothing, so nothing passes through C: \(\eta_C = 0\).
- Load on CD (\(440 \le x \le 690\)): CD is a simple beam between the two hinges, and each hinge takes its lever-rule share: \(\eta_C = (690-x)/250\), from 1 at C to 0 at D.
- Load on DEF (\(x \gt 690\)): the mirror of the first case. The load goes to E and F, CD stays unloaded, and \(\eta_C = 0\).
- Load pada ABC (\(x \lt 440\)): ABC berdiri atas support-nya sendiri, A dan B, dan membawa load terus kepadanya. Suspended span tidak membawa apa-apa, jadi tiada daya melalui C: \(\eta_C = 0\).
- Load pada CD (\(440 \le x \le 690\)): CD ialah simple beam antara dua hinge, dan setiap hinge mengambil bahagiannya mengikut lever rule: \(\eta_C = (690-x)/250\), dari 1 di C hingga 0 di D.
- Load pada DEF (\(x \gt 690\)): cermin kes pertama. Load pergi ke E dan F, CD kekal tidak dibebani, dan \(\eta_C = 0\).
The jump at C. Just left of C the load stands on the cantilever tip, which belongs to ABC, so it goes straight to A and B and \(\eta_C = 0\). Just right of C it stands on the suspended span at its support, so the whole load passes through the hinge and \(\eta_C = 1\). Müller–Breslau gives the same picture: cut the vertical connection at C and lift the end of CD by 1 relative to the tip. ABC does not move, because A and B still support it; CD rotates about D. Select RC in the demonstration in Section 4 to see it.Lompatan di C. Sedikit di kiri C, load berada di hujung cantilever yang merupakan sebahagian daripada ABC, jadi ia terus ke A dan B dan \(\eta_C = 0\). Sedikit di kanan C, load berada pada suspended span di support-nya, jadi seluruh load melalui hinge dan \(\eta_C = 1\). Müller–Breslau memberi gambaran yang sama: potong sambungan menegak di C dan angkat hujung CD sebanyak 1 relatif kepada hujung cantilever. ABC tidak bergerak kerana A dan B masih menyokongnya; CD berputar terhadap D. Pilih RC dalam demonstrasi di Section 4 untuk melihatnya.
A mass stands at halt 3 (x = 300 mm, on the cantilever BC). The gauge at C reads …Satu jisim berada di halt 3 (x = 300 mm, pada cantilever BC). Gauge di C membaca …
The load is on ABC, which carries it to A and B by itself. The suspended span is unloaded, so nothing passes through hinge C.Load berada pada ABC, yang membawanya ke A dan B dengan sendirinya. Suspended span tidak dibebani, jadi tiada daya melalui hinge C.
Step 5 · Assemble and checkLangkah 5 · Gabung dan semak
Three checks catch most mistakes: (i) \(\eta_A+\eta_B+\eta_E+\eta_F = 1\) for every \(x\); (ii) the two formulae agree at the hinges; (iii) the slopes are \(-1/250\) per mm on ABC and \(+0.76/250\) on CD, and a kink can occur only at a hinge, never at B, which lies inside the rigid beam ABC.Tiga semakan menangkap kebanyakan kesilapan: (i) \(\eta_A+\eta_B+\eta_E+\eta_F = 1\) bagi setiap \(x\); (ii) dua formula bersetuju di hinge; (iii) slope ialah \(-1/250\) per mm pada ABC dan \(+0.76/250\) pada CD, dan bengkokan hanya boleh berlaku di hinge, tidak sekali-kali di B, yang terletak di dalam rigid beam ABC.
A unit load stands at the tip C. What is \(\eta_B\)?Unit load berada di hujung C. Berapakah \(\eta_B\)?
\(\eta_B(440) = 440/250 = 1.76\): B carries the load and also balances the pull-down at A.\(\eta_B(440) = 440/250 = 1.76\): B membawa load dan juga mengimbangi tarikan ke bawah di A.
4 The Müller–Breslau principle4 Prinsip Müller–Breslau
Key pointsIsi penting
- Release the restraint, impose a unit displacement: the deflected shape is the influence line.
- Exact ordinates for determinate structures (rigid links); shape only for indeterminate ones.
- Kinks only at hinges and at the released restraint.
- Lepaskan restraint, kenakan unit displacement: deflected shape ialah influence line.
- Ordinate tepat bagi struktur determinate (rigid link); bentuk sahaja bagi struktur indeterminate.
- Bengkokan hanya di hinge dan di restraint yang dilepaskan.
For \(R_A\): remove the support at A and lift that end by one unit. Beam ABC is rigid between its support and the hinge, so it rotates about B: A rises by 1 and the tip C, 190 mm on the other side of B, drops by \(190/250 = 0.76\). The suspended span follows C and stays straight, dropping linearly to zero at D; beam DEF does not move. The result is exactly the influence line of Section 3, signs included.
Bagi \(R_A\): buang support di A dan angkat hujung itu sebanyak satu unit. Beam ABC adalah rigid antara support dan hinge, jadi ia berputar terhadap B: A naik sebanyak 1 dan hujung C, 190 mm di sebelah lain B, turun sebanyak \(190/250 = 0.76\). Suspended span mengikut C dan kekal lurus, turun secara linear ke sifar di D; beam DEF tidak bergerak. Hasilnya tepat sama dengan influence line dalam Section 3, termasuk tanda.
Two remarks. The principle gives exact ordinates only for statically determinate structures, where the released structure is a mechanism of straight rigid links; for an indeterminate beam the released structure bends and the principle gives the shape only. And the kinks of the deflected shape lie at the hinges and at the released restraint, never inside a rigid member: a quick visual check of any influence line you compute.
Dua catatan. Prinsip ini memberi ordinate yang tepat hanya bagi struktur statically determinate, di mana released structure ialah mechanism yang terdiri daripada rigid link yang lurus; bagi beam indeterminate, released structure melentur dan prinsip ini hanya memberi bentuk. Selain itu, bengkokan pada deflected shape terletak di hinge dan di restraint yang dilepaskan, tidak sekali-kali di dalam anggota rigid: semakan visual yang pantas bagi mana-mana influence line yang anda kira.
Release B and lift it by 1. Beam ABC rotates about A. The tip C …Lepaskan B dan angkat sebanyak 1. Beam ABC berputar terhadap A. Hujung C …
A rigid bar pinned at A and lifted by 1 at 250 mm rises in proportion to the distance from A: \(440/250 = 1.76\) at C, the peak of \(\eta_B\).Bar rigid yang di-pin di A dan diangkat 1 pada 250 mm naik berkadar dengan jarak dari A: \(440/250 = 1.76\) di C, iaitu puncak \(\eta_B\).
5 Using an influence line5 Menggunakan influence line
Key pointsIsi penting
- \(R = \sum P_i\,\eta_R(x_i)\); for a UDL, \(R = w\times\) area under the line.
- Piecewise-linear lines: the extreme of a load train occurs with one load on a vertex.
- Compound load of Test 2: most negative \(R_A = -4.94\) kgf with the 5 kg mass at C.
- A UDL over the whole model gives \(R_A = -42.2\,w\): the deck lifts at A.
- \(R = \sum P_i\,\eta_R(x_i)\); bagi UDL, \(R = w\times\) area di bawah garis.
- Garis piecewise linear: nilai ekstrem bagi load train berlaku apabila satu load berada pada vertex.
- Compound load Test 2: \(R_A\) paling negatif \(= -4.94\) kgf dengan jisim 5 kg di C.
- UDL pada seluruh model memberi \(R_A = -42.2\,w\): deck terangkat di A.
By superposition, for a single load \(P\) at \(x_1\), a series of loads \(P_i\) at \(x_i\), and a uniformly distributed load \(w\) between \(a\) and \(b\):
Melalui superposition, bagi satu load \(P\) di \(x_1\), satu siri load \(P_i\) di \(x_i\), dan uniformly distributed load \(w\) antara \(a\) dan \(b\):
\[ R = P\,\eta_R(x_1),\qquad R = \sum_i P_i\,\eta_R(x_i),\qquad R = \int_a^b w\,\eta_R(x)\,\mathrm{d}x = w\times(\text{area under the IL from } a \text{ to } b). \]With masses in kg the reactions come out in kgf, which is what the laboratory gauges read.
Dengan jisim dalam kg, reaction yang diperoleh dalam kgf, iaitu unit bacaan gauge makmal.
5.1 Critical position of a series of loads5.1 Critical position bagi satu siri load
Every influence line of the model is piecewise linear, so \(\sum_i P_i\,\eta_R(x_i)\) is a piecewise linear function of the position of the load group, and a piecewise linear function reaches its extremes at a vertex. The largest (or most negative) value therefore occurs when one of the loads stands on a vertex of the influence line; only a few positions need to be tried.
Setiap influence line model ini adalah piecewise linear, jadi \(\sum_i P_i\,\eta_R(x_i)\) ialah fungsi piecewise linear terhadap kedudukan kumpulan load, dan fungsi piecewise linear mencapai nilai ekstrem pada vertex. Nilai terbesar (atau paling negatif) oleh itu berlaku apabila salah satu load berada pada vertex influence line; hanya beberapa kedudukan perlu dicuba.
Worked example 1 · The compound load of Test 2Worked example 1 · Compound load bagi Test 2
The 5 kg mass stands at a halt and the 2.5 kg mass 100 mm to its right; the pair moves to the right, so the 2.5 kg mass is in front. With the 5 kg mass at \(x\):Jisim 5 kg berada pada satu halt dan jisim 2.5 kg 100 mm di sebelah kanannya; pasangan ini bergerak ke kanan, jadi jisim 2.5 kg berada di hadapan. Dengan jisim 5 kg di \(x\):
\[ R_A(x) = 5\,\eta_A(x) + 2.5\,\eta_A(x+100)\quad\text{(kgf)}. \]5 kg mass at A: \(R_A = 5(1.0)+2.5(0.6) = 6.5\) kgf. 5 kg mass at C: \(\eta_A(540) = -0.76\times(690-540)/250 = -0.456\), so \(R_A = -3.80 - 1.14 = -4.94\) kgf. 2.5 kg mass at C (5 kg mass at 340 mm): \(R_A = 5(-0.36) + 2.5(-0.76) = -3.70\) kgf. The most severe pull-down at A occurs with the heavier load on the vertex C. The largest \(R_B\), 11.44 kgf, is more than 1.5 times the total mass of 7.5 kg.Jisim 5 kg di A: \(R_A = 5(1.0)+2.5(0.6) = 6.5\) kgf. Jisim 5 kg di C: \(\eta_A(540) = -0.76\times(690-540)/250 = -0.456\), maka \(R_A = -3.80 - 1.14 = -4.94\) kgf. Jisim 2.5 kg di C (jisim 5 kg di 340 mm): \(R_A = 5(-0.36) + 2.5(-0.76) = -3.70\) kgf. Tarikan ke bawah paling teruk di A berlaku apabila load yang lebih berat berada pada vertex C. \(R_B\) terbesar, 11.44 kgf, melebihi 1.5 kali jumlah jisim 7.5 kg.
5.2 Distributed load: area under the influence line5.2 Distributed load: area di bawah influence line
The areas under \(\eta_A\) are, by the triangle rule, \(+\tfrac12(250)(1.0) = +125\) mm over AB, \(\tfrac12(190)(-0.76) = -72.2\) mm over BC and \(\tfrac12(250)(-0.76) = -95.0\) mm over CD, and zero over DEF.
Area di bawah \(\eta_A\), menggunakan petua segi tiga, ialah \(+\tfrac12(250)(1.0) = +125\) mm pada AB, \(\tfrac12(190)(-0.76) = -72.2\) mm pada BC dan \(\tfrac12(250)(-0.76) = -95.0\) mm pada CD, dan sifar pada DEF.
Worked example 2 · A uniformly distributed loadWorked example 2 · Uniformly distributed load
A load \(w = 0.01\) kg/mm (2.5 kg spread over 250 mm): over AB only, \(R_A = 0.01\times125 = 1.25\) kgf (half the load, as for a simple span); over BC and CD, \(R_A = 0.01\times(-167.2) = -1.67\) kgf; over the whole model, \(R_A = 0.01\times(125-72.2-95.0) = -0.42\) kgf. A bridge of this type loaded uniformly along its whole length lifts at A, and the support must be able to hold the deck down.Load \(w = 0.01\) kg/mm (2.5 kg tersebar atas 250 mm): pada AB sahaja, \(R_A = 0.01\times125 = 1.25\) kgf (separuh load, seperti simple span); pada BC dan CD, \(R_A = 0.01\times(-167.2) = -1.67\) kgf; pada seluruh model, \(R_A = 0.01\times(125-72.2-95.0) = -0.42\) kgf. Jambatan jenis ini yang dibebani secara seragam sepanjang keseluruhannya akan terangkat di A, dan support mesti mampu menahan deck ke bawah.
Check by staticsSemakan dengan statik
Beam ABC carries \(w(250+190)\) directly plus half the suspended span, \(125w\), at C. Moments about B:Beam ABC membawa \(w(250+190)\) secara terus ditambah separuh suspended span, \(125w\), di C. Moment terhadap B: \(R_A\cdot250 = 250w(125) - 190w(95) - 125w(190) = -10\,550\,w\), somaka \(R_A = -42.2\,w\), the same as the area., sama dengan area.
For a train of loads on a piecewise-linear influence line, the extreme response occurs when …Bagi load train pada influence line yang piecewise linear, response ekstrem berlaku apabila …
The sum is piecewise linear in the position of the train, so its extremes are at breakpoints: one load on a vertex.Jumlahnya piecewise linear terhadap kedudukan load train, jadi nilai ekstremnya berada pada breakpoint: satu load pada vertex.
6 The experiment and its data reduction6 Eksperimen dan data reduction
Key pointsIsi penting
- \(\eta_{\text{test}} = \text{reading}\times0.05/m\), with \(m = 2.5\) kg in Test 1.
- Compare by absolute difference; percentages only where the ordinate is large.
- Equilibrium check at every halt: \((a+b+e+f)\times0.05 \approx 2.5\) kgf.
- \(\eta_{\text{test}} = \text{reading}\times0.05/m\), dengan \(m = 2.5\) kg dalam Test 1.
- Bandingkan dengan perbezaan mutlak; peratusan hanya apabila ordinate besar.
- Equilibrium check pada setiap halt: \((a+b+e+f)\times0.05 \approx 2.5\) kgf.
What is measured. A 2.5 kg mass is placed at each of the seventeen halts in turn (Test 1), then the 5 kg + 2.5 kg pair (Test 2). At each halt the six dial gauges are read. One division corresponds to 0.05 kgf, so the experimental ordinate per unit load is
Apa yang diukur. Jisim 2.5 kg diletakkan pada setiap tujuh belas halt secara bergilir (Test 1), kemudian pasangan 5 kg + 2.5 kg (Test 2). Pada setiap halt, enam dial gauge dibaca. Satu division bersamaan 0.05 kgf, jadi ordinate eksperimen per unit load ialah
\[ \eta_{\text{test}} = \frac{(\text{reading in divisions})\times 0.05}{m},\qquad m = 2.5\ \text{kg (Test 1)}. \]For Test 2, reading × 0.05 is the reaction in kgf, comparable with the compound-load table.
Bagi Test 2, bacaan × 0.05 ialah reaction dalam kgf, boleh dibandingkan dengan jadual compound load.
How to compare. Report the difference \(\eta_{\text{test}}-\eta_{\text{theory}}\) at every halt. A percentage difference is meaningful only where the theoretical ordinate is not small: at halt 2, where \(\eta_A = 0.2\), a gauge error of one division (0.02 per unit load) is already 10 %, and where the theoretical value is zero the percentage is undefined. Judge the agreement by the absolute difference and by the shape of the line.
Cara membandingkan. Laporkan perbezaan \(\eta_{\text{test}}-\eta_{\text{theory}}\) pada setiap halt. Perbezaan peratusan hanya bermakna apabila ordinate teori tidak kecil: di halt 2, di mana \(\eta_A = 0.2\), error gauge satu division (0.02 per unit load) sudah 10 %, dan apabila nilai teori sifar, peratusan tidak tertakrif. Nilai persetujuan berdasarkan perbezaan mutlak dan bentuk garis.
Equilibrium check. With the mass at any halt the four support gauges should add up to the applied mass: \((a+b+e+f)\times0.05 \approx 2.5\) kgf. Check it before leaving the laboratory, while the readings can still be repeated. The Lab tab does this for you.
Equilibrium check. Dengan jisim di mana-mana halt, jumlah bacaan empat support gauge sepatutnya sama dengan jisim yang dikenakan: \((a+b+e+f)\times0.05 \approx 2.5\) kgf. Semak sebelum keluar makmal, ketika bacaan masih boleh diulang. Tab Makmal melakukannya untuk anda.
7 Sources of error7 Sumber error
Key pointsIsi penting
- Placement ±5 mm and gauge ±1 division each give about ±0.02 per unit load.
- Combined in quadrature: about ±0.03, the same at every halt.
- That is 3 % at A but 15 % at halt 2: use absolute differences.
- Kedudukan ±5 mm dan gauge ±1 division masing-masing memberi lebih kurang ±0.02 per unit load.
- Digabung secara quadrature: lebih kurang ±0.03, sama pada setiap halt.
- Itu 3 % di A tetapi 15 % di halt 2: guna perbezaan mutlak.
| SourceSumber | EstimateAnggaran | Effect onKesan pada \(\eta_A\) |
|---|---|---|
| Mass placed ±5 mm from the haltJisim diletak ±5 mm dari halt | slope × Δx: (1/250)(5) on ABC, (0.76/250)(5) on CD | ±0.020; ±0.015 |
| Gauge resolution, ±1 divisionResolusi gauge, ±1 division | 0.05/2.5 | ±0.020 |
| Zero drift between readingsZero drift antara bacaan | re-zero after each halt; otherwise 1–2 divisionsre-zero selepas setiap halt; jika tidak, 1–2 division | ±0.02–0.04 |
| Friction in hinges and gaugesGeseran dalam hinge dan gauge | systematic; lowers the sum of the support readingssistematik; merendahkan jumlah bacaan support | see the sum checklihat semakan jumlah |
Combining the first two in quadrature gives about ±0.03 per unit load, the same at every halt. Against an ordinate of 1.0 at A this is 3 %; against 0.2 at halt 2 it is 15 %. That is the quantitative reason for comparing by absolute difference.
Menggabungkan dua yang pertama secara quadrature memberi lebih kurang ±0.03 per unit load, sama pada setiap halt. Berbanding ordinate 1.0 di A, ini 3 %; berbanding 0.2 di halt 2, ia 15 %. Itulah sebab kuantitatif untuk membandingkan dengan perbezaan mutlak.
The theoretical ordinate is 0.20 and the uncertainty is ±0.03. The percentage difference a perfect experiment could still show is up to …Ordinate teori ialah 0.20 dan uncertainty ±0.03. Perbezaan peratusan yang masih boleh ditunjukkan oleh eksperimen yang sempurna ialah sehingga …
\(0.03/0.20 = 0.15\). The same ±0.03 is only 3 % of the ordinate at A.±0.03 yang sama hanya 3 % daripada ordinate di A.
8 Beyond the laboratory8 Di luar makmal
Key pointsIsi penting
- Bridge design places standard vehicle and lane loads using influence lines or surfaces.
- Continuous girders have curved lines; Müller–Breslau still shows which spans to load.
- Gerber bridges: forces by statics alone, at the price of end supports designed for uplift.
- Rekabentuk jambatan meletakkan standard vehicle load dan lane load menggunakan influence line atau influence surface.
- Continuous girder mempunyai garis melengkung; Müller–Breslau masih menunjukkan span mana yang perlu dibebani.
- Gerber bridge: daya diperoleh dengan statik sahaja, dengan harga end support yang perlu direka untuk uplift.
Bridge decks are designed for standard vehicle and lane loads placed, by means of influence lines or influence surfaces, where they produce the largest effects at each section. For continuous (indeterminate) girders the influence lines are curved and need an elastic analysis, but the Müller–Breslau sketch still tells the engineer which spans to load. The cantilever bridge, with its determinate hinges, made the long steel spans of the late nineteenth century possible because its forces could be found by statics alone; the price is end supports that must be designed for uplift, as Worked example 2 shows.
Deck jambatan direka untuk standard vehicle load dan lane load yang diletakkan, menggunakan influence line atau influence surface, di kedudukan yang menghasilkan kesan terbesar pada setiap section. Bagi continuous girder (indeterminate), influence line melengkung dan memerlukan analisis elastik, tetapi lakaran Müller–Breslau masih memberitahu jurutera span mana yang perlu dibebani. Cantilever bridge, dengan hinge yang determinate, membolehkan span keluli yang panjang pada akhir abad kesembilan belas kerana dayanya boleh dicari dengan statik sahaja; harganya ialah end support yang mesti direka untuk uplift, seperti yang ditunjukkan dalam Worked example 2.
SummaryRingkasan
\(\eta_A = (250-x)/250\) onpada ABC, \(-0.76\,\eta_C\) onpada CD, 0 onpada DEF; \(\eta_B = x/250\) onpada ABC, \(1.76\,\eta_C\) onpada CD.
\(\eta_C = (690-x)/250\), \(\eta_D = (x-440)/250\) on CD, zero elsewhere;pada CD, sifar di tempat lain; \(\eta_E\), \(\eta_F\) mirrorialah imej cermin \(\eta_B\), \(\eta_A\). Check:Semakan: \(\eta_A+\eta_B+\eta_E+\eta_F = 1\).
\(R = \sum P_i\,\eta_R(x_i)\); for a distributed loadbagi distributed load \(R = w\times\) area. The extreme of a load train occurs with one load on a vertex.Nilai ekstrem load train berlaku dengan satu load pada vertex.
\(\eta_{\text{test}} = \text{reading}\times0.05/m\); compare by absolute difference; quote percentages only at large ordinates.bandingkan dengan perbezaan mutlak; nyatakan peratusan hanya pada ordinate besar.
ReferencesRujukan
Hibbeler, R. C. (2018). Structural Analysis, 10th ed. Pearson, chapter 6.
Kassimali, A. (2020). Structural Analysis, 6th ed. Cengage, chapter 8.
Müller-Breslau, H. (1886). Die neueren Methoden der Festigkeitslehre und der Statik der Baukonstruktionen. Leipzig.
Faculty of Civil Engineering, UTM (2026). Civil Engineering Laboratory II: Laboratory Manual and Data Sheets, experiment S2.