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Tentamen 7 November 2016, antwoorden

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Mechanics (NAMECH05E)

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Problem 1

:

y

p

p

AI

t 1

1

as

.

1 O

k N

1

o

KN

20 KN

b)

A

a

= 0

, Ay

Gy

=

(

w + 20 +

io

)

KN

For eoint

A

.

Gt

Ta

MA to

Gy

.

12 m

  • 10 KN

. 8m

20

KN

. Gm

  • / o

KN.

4m=O

Gy

= 20

KN

{

Ay

= 20 KN

C)

Method

of

joints

.

.

If

the

entire

truss is at

equilibrium

then each

joint

must

he in

equilibrium

Method

of

section

.

.

If

the

entire

truss is at

equilibrium

then each member

must

he in

equilibrium

d) For

joint

A

TT

tFy=O

;

20 -

Fay

sin

450=

FAL

=

KN

→ I7x=

5

FAB

28 Cos 450=

Faa

=

20 KN

Y

KIM

A

g-

FAB

,

ZOKN

For the

joint

L

\y+

ZFr=

FLC =o

fuc

Y

; Fe

null

Try

=o

FLK

=O

\*Ee

FLK

= 28 KN

FLAE

KN

2C

For the

joint

K

y

t Its

-

;

kμ•#g

FKT

1°sin45°

7k

,

cos

(450-26)=

¢§o

null

°

FKD =

KN (

compression )

FKL

28

μ p

2C

10kW

KD

A

IFy=

;

locos 450 + 7 (

450-26.

)

Fky

=O

Fks

=

kW

Plastic

deformation

:

Py

=

6ypr2=

. q

|°'2zI

)

=

17

. ,

MN

Stable

structures for

all members

,

no

bucketing

& Hastie

Deformation

Problem

2

y

A)

ooh

My

x

y

the

oee↳⇒tkaEee*

.

g

Z

KIEIFEEEHI

'm

asm

E

Z

ten

.

b)

front

section

M

,

back

section

M

M=5KN

.

  1. =

15km m

c

)

Fy

=o =

Vy

  • 5

(

¥

) = 0

Vy

= 3kW

Fz

= o = Vz

  • 5

(

¥

) =

o Vz

=

  • 4kW

2-

My

=

0

My

5(4z)

to.

=o

My

=

KN. in

I

Mz = 0

MZ

5( ¥

) 10=0 Mz =

KN . m

Iy

=

Iz

=

####### EN

=

¥

( o

4

=

2 ×

co

m

o =

the

Mtfzy

Bending

cause

only

she

normal stress

forrpoinf A

,

Y=

0

,

-2=

g=

μZY_

  • 0

Iz

=

0×03 N. m

to

.o4m

)

0×(10-6) a-

my

= -

17

'9MPa

=

17

for

point

Is

Y=

0

,

2=0.

on

Myz

J

=

0 +

Ly

=

N. M

(

0 ' 04h

)

=

23

d)

,

  1. ×

Cio

  1. Ti

m

a

-27g

'

  • 0

Try

'=

FM

I

Mz•=O

Mz

'

  • F

N.

o .5m= 0

M

¥¥↳

,

Mz

"

=

Fm

N .

in

p

.

MZY

Myz

'

r

=

t -

Iz

'

Iy

'

Iz

'=Iy'

=I£=Iy

=

qtr

4

TM =

Mz

'

y

"

null

0 =

350

MPA

,

Mz

'

isthemaxmium

of

bending

moment

Problem 3

a)

W

B.

••c

p

p

RA

RB

b)

RAT RB=

W

W

= Zoo

kg

.

9%

=

i. KN

Dmeto

symmetric

structure

RA = RB

=

o/kN

c)

,

yeti

:*

§ }

Np

Ne (

String

)

(

Vessel

)

Cy

Cy

b/c•t→c×

a

,

fd

t

← •o

N

't

@

ight

leg

)

(

Left

leg ) ,

I

RB

Rap

C

T

To - the

vessel

-27×-0 Nb

cos

45°

N

cos

450 = 0

No =

Nz

  • P

IFY

=o

N

,

sin 450

Nesin

450

W

= 0

fz Np

= W

Np

= NE

=

IZW

=

EZ

.

i.

KN

=

387

KN

choose one side

of

The stand

=

Say

BC

Cy

No

/c•$→c×

heft

leg

PRB

T

IF

=

o

Nbsim45° + Cx

T

=

0 @

  • T

Try

= o

Nd

cos 450 +

Cy

RB =o

@

Me =o

choose

point

C as

origin

RB

. In + T

'

In

ND

.

  1. m=O

3

f)

TL 2090.

N

.

= - 2nd

=

EA

2° x.

09dg

.

T,

.co#mr=6

=

66μm

0

=

IA

= 6.

Mpa

< Goo

Mpa

,

So

, safe

structure

,

no plastic

deformation expected

Considering

the

following

ratio

foo Mpa

:

Wmax Goo

Wmax

⇒ -

  1. 655

Mpa

: W

=

KN

Wmax

= 176,

KN

corresponding

to

18031kg

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Tentamen 7 November 2016, antwoorden

Vak: Mechanics (NAMECH05E)

27 Documenten
Studenten deelden 27 documenten in dit vak
Was dit document nuttig?
Problem 1
:
y
pp
AI t11as
.
1OkN1oKN
20 KN
b) Aa=0,Ay +Gy =(w +20 +io )KN
For eoint A.Gt Ta MA to
Gy .12 m-10 KN .8m -20 KN .Gm -/oKN .4m=O
Gy =20 KN
{Ay =20 KN
C) Method of joints .
.If the entire truss is at equilibrium
then each joint must he in equilibrium
Method of section .
.If the entire truss is at equilibrium
then each member must he in equilibrium