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Fig. 5. Spatial distribution of pressure (

a

) and temperature (

b

) at the moment

t

= 9

.

1

ms (Experiment 4):

1

— shock-compressed test (driven) gas behind the reflected shock wave;

2

— reflected

shock wave front;

3

— area of the initial shock-compressed test (driven) gas;

4

— contact

boundary front;

5

— space occupied by the rarefaction wave in driver gas

the most significant peculiarity of the interaction of a shock wave with

a solid barrier is the shock wave amplification after its reflection from

the barrier [10]. It is convenient to characterize the process of the shock

wave reflection by the relative amplification coefficient:

K

=

Δ

p

3

Δ

p

2

, where

Δ

p

3

=

p

3

p

1

is the excessive pressure in the reflected shock wave,

Δ

p

2

=

p

2

p

1

is the excessive pressure in the incident wave.

From graphic curves given in Fig. 3, it follows that the shock wave

collision with the solid barrier results in the appreciable amplification of

the reflected shock wave: the amplification coefficient

K

6

(for air the

maximum value of amplification coefficient is

K

= 8)

. The amplitude

value of the reflected shock wave

Z

24

, the temperature and pressure

at the right computed boundary increase to

T

1

.

2

кK,

p

3

.

5

atm.

By this moment, the fan-shaped flow of rarefaction waves has already

reflected from the left computed boundary and moved more than half into

the computed zone. Along with it, the temperature and pressure at the left

boundary have dropped to

T

0

.

2

кK,

p

7

atm.

Then, mostly at the right computed boundary, we can observe the flow

structure (Fig. 6) corresponding to the phase of complex interaction of the

shock wave, contact discontinuity, and rarefaction wave, which expands

approximately for

10

.

3

6

t

6

10

.

3+

L

HP c

+

L

LP c

c

1

35

ms. The reflected

shock wave interacts only with the contact discontinuity that moves towards

it at the initial stage of the phase of flowing in the shock tube in the vicinity

of the right computed boundary.

In this case there can be two options of the interaction: a) if the shock

wave interacting with the contact discontinuity expands from the denser

ISSN 0236-3941. HERALD of the BMSTU. Series “Mechanical Engineering”. 2014. No. 1 19