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The Influence of the Supply Chamber Configuration on Under-Expanded Swirling Jets

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(1)

⏎㯦 㺪⻚ 䡫㌗㧊 ⿖㫇䖓㺓 㓺㤪㩲䔎 㥶☯㠦 ⹎䂮⓪ 㡗䟻㠦 ὖ䞲 㡆ῂ

卆渗愶 ̐ · 決劒籲* · 皦柢橊疪 显皦割獞** · 卆籲壟***

The Influence of the Supply Chamber Configuration on Under-Expanded Swirling Jets

Jung-Bae Kim, Kwon-Hee Lee, Toshiaki Setoguchi and Heuy-Dong Kim

Key Words : Supersonic swirling jet(㽞㦢㏣ 㓺㤪㩲䔎), Supply chamber configuration(Ὃ  㺪⻚䡫

㌗), Shock wave(㿿ỿ䕢), Recirculation Zone(㨂㑲䢮 㡗㡃)

Abstract

The present study addresses experimental results to investigate the effect of the jet supply chamber configuration on the sonic/supersonic swirling jets, as the case study. The experiment is carried out using the convergent nozzle with a various different chamber configurations upstream the nozzle throat, which is composed of four tangential inlet holes for the swirling flows. The jet pressure ratio is varied between 3.0 and 7.0. The sonic/supersonic swirling jet flows are specified by the pitot impact and static pressure measurements and visualized using the Shadowgraph method. The results show that the major structures of the sonic/supersonic swirling jet are strongly influenced by the jet supply chamber.

1. 昢 嵦

㦢㏣/㽞㦢㏣ 㓺㤪㩲䔎⓪ 㠪㰚 㡆㏢㔺 㩲䔎 ㏢㦢 ἓṦ, ⚦ 㥶☯㦮 䢒䞿㎇⓻ ⹥ 㩞┾㎇⓻ 䟻㌗, 㡆㏢

㔺⌊㦮 䢪㡒 㞞㩫 ❇ 㡂⩂ ㌆㠛 ⿚㟒㠦㍲ ⍦Ⰲ 㧊 㣿♮ἶ 㧞┺. 㓺㤪㩲䔎⓪ 㩲䔎⌊㠦㍲ 㿿ỿ䕢Ṗ ⹲

㌳䞮Ệ⋮, 㥶㼊㦮 䣢㩚㤊☯ὒ ⋲⮮ 㥶☯㦮 ⽋䞿㩗 㧎 ₆㼊㡃䞯㩗 䔏㎇㦚 Ṗ㰚 䣢㩚㤊☯㧊 ⏎㯦㌗⮮

㠦㍲ 㭒㠊㰞 ➢ ⹲㌳䞮Ⳇ, ⏎㯦⪲⿖䎆 ⹿㿲♮⓪

₆㼊㥶☯㦖 ゚㓺㤪㩲䔎 㥶☯ὒ⓪ ╂Ⰲ, 㿫⹿䟻 ⹥

⹮ἓ⹿䟻 ㏣☚ ㎇⿚ ㈦Ⱒ 㞚┞⧒ ⻫㍶⹿䟻 ㏣☚

㎇⿚㦚 Ṗ㰖Ợ ♲┺. 㰖⁞₢㰖 㓺㤪㩲䔎㠦 ╖䞲 Ⱔ㦖 㡆ῂṖ 㑮䟟♮㠞㦒Ⳇ, 㧊✺㦮 㡆ῂ㠦 ➆⯊Ⳋ,

㓺㤪㩲䔎⓪ ゚㓺㤪㩲䔎㠦 ゚䟊 㭒㥚 ₆㼊㦮 㩲䔎

⌊⿖⪲㦮 䢒㧛㦚 㯳Ṗ㔲䅲 㩲䔎 䆪㠊㦮 ₎㧊⯒ Ṧ

㏢㔲䋾┺ἶ ⽊ἶ䞮㡖┺. (1,2) ⡦䞲 㓺㤪 ṫ☚(swirl intensity)⓪ 㓺㤪㩲䔎㦮 䔏㎇㦚 ἆ㩫䞮⓪ 㭒㣪䞲

⼖㑮⧒⓪ ộ㧊 㞢⩺㪢㦒Ⳇ, 㓺㤪ṫ☚Ṗ 㧚ἚṨ㦚 㽞ὒ䞮Ⳋ 㓺㤪㩲䔎 㭧㕂㿫 ⿖⁒㠦 㡃㞫⩻ ῂ⺆㡗 㡃㧊 㫊㨂䞮Ợ ♲┺ (3) . 㧊⪲ 㧎䞮㡂 ⹲㌳䞮⓪ 㨂㑲 䢮㡗㡃㦖 㡆㏢㔺⌊㦮 䢪㡒㞞㩫ὒ ⹖㩧䞲 ὖἚ⯒

Ṗ㰖ἶ 㧞㠊 㭒㣪䞲 㡆ῂ╖㌗㧊 ♮㠊 㢪┺. ⡦䞲 㧊⩂䞲 㓺㤪㥶☯㦚 ⹲㌳㔲䋺₆ 㥚䞮㡂 Ⱔ㦖 ⹿⻫

㧊 㡆ῂ♮㠊㪢㦒Ⳇ, ╖䚲㩗㧎 ộ㦒⪲ ⻫㍶⹿䟻 㥶 㧛ῂ ⹥ 㩗╏䞲 ⻶㧎(vane)㦚 ㌂㣿䞮Ệ⋮ (4) , 䣢㩚 㧊 Ṗ⓻䞲 㥶㧛ῂ㦮 ㌂㣿 (5) , 㿫⹿䟻 ⹥ 㩧㍶⹿䟻㦮 㓺㤪 ⹲㌳₆ (6) , ⁎Ⰲἶ な⩞㧊✲ (7) . ❇㧊 ㌂㣿♮ἶ 㧞┺. 㽞㦢㏣ 㓺㤪㩲䔎㠦 ╖䞲 㡆ῂ⪲⓪ Carpenter (8,9) Ṗ 㧒㹾㤦 㧊⪶ 䟊㍳㦚 ㌂㣿䟊 ⧒⹲⏎

㯦㠦㍲ ⹲㌳♮⓪ 㽞㦢㏣ 㓺㤪㩲䔎 䔏㎇㦚 Ἒ㌆䞮 㡖┺. ⁎ἆὒ 㓺㤪㧊 ⏎㯦㦮 ⳿(㰞㔳 㫆Ị)㦚 ₆㭖 㦒⪲ ⏎㯦 ⌊⿖ 㥶☯ὒ 㣎⿖ 㡃⮮㥶☯㦒⪲ ⋮⑚㰦 㦚 䢫㧎䞮㡖㦒⋮ ⏎㯦㦮 䡫㌗, 㓺㤪ṫ☚ ❇㦮 ┺ 㟧䞲 ⿚㍳㦖 㧊⬾㠊 㰖㰖 㞠㞮┺. Dutton (10) 㦖 㽞

̐ 㞞☯╖䞯ᾦ ₆ἚὋ䞯ὒ ╖䞯㤦 E-mail : [email protected]

TEL : (054)820-5622 FAX : (054)823-5495

* ㌂Ṗ╖䞯ᾦ ₆ἚὋ䞯ὒ ╖䞯㤦, 㧒⽎

** ㌂Ṗ╖䞯ᾦ ₆ἚὋ䞯ὒ, 㧒⽎

*** 㞞☯╖䞯ᾦ ₆ἚὋ䞯⿖

(2)

㦢㏣ ⏎㯦⌊ 㥶☯㠦㍲ ⏎㯦䡫㌗, 㧛ῂ 㓺㤪 䡫㌗,

⹥ 㓺㤪 ṫ☚㦮 㡗䟻㠦 ὖ䞮㡂 㫆㌂䞮㡖┺.

㾲⁒㠦 Culter ❇ (11) 㦖 ⏎㯦 ⌊⿖㠦 㤷㧊⋮ ⻶㧎 㦚 ㍺䂮䞮㡂 㓺㤪㩲䔎⋮ 㢖⮮⯒ ⹲㌳㔲䋺⓪ 㧊㩚 㦮 ⹿⻫⽊┺ 㿫㏢䢫╖ ⏎㯦㦮 㥶㧛ῂ㠦 㩧㍶⹿䟻 㦮 㓺㤪⩂⯒ ㌂㣿䞮⓪ ộ㧊 ▪ ⏨㦖 䞒䋂 helix angle ⯒ ⹲㌳㔲䋺ἶ 㥶☯ 䢒䞿㠦 䣾㥾㩗㧊┺⓪ ộ 㦚 ⽊ἶ䞮㡖┺. ⡦䞲, Yu ❇ (12) 㦖 㩧㍶⹿䟻 㥶㧛ῂ 㠦 㦮䟊 ⹲㌳䞮⓪ 㓺㤪㥶☯㦖 㩲䔎㦮 㿿ỿ䕢㏢㦢 㦚 Ṧ㏢㔲䋺⓪◆ 䣾ὒṖ 㧞㦢㦚 ⹳䡪┺. ⁎⩂⋮, 㧒⹮㩗㦒⪲ 㧊⩂䞲 ⏎㯦㦚 ㌂㣿䞮⓪ 㡆ῂ㠦㍲, ⏎ 㯦 ㌗⮮ 㩫㼊 㡗㡃 䔏㎇㦚 䁷㩫䞮₆ 㥚䟊 ⏎㯦⌊

⿖㠦⓪ 㩫㞫Ὃ, 䞒䏶 䝚⪲ぢ ⹥ 㤦䐋䡫㦮 㡊㩚╖

(thermocouple) ❇㧊 ㌂㣿♮ἶ 㧞┺. 䡚㨂₢㰖, ⏎ 㯦㦚 䐋䞮⓪ 㿎䋂♲ 㥶☯㦮 㩲䔎 ῂ㫆⓪ ┾㰖 ㌗

⮮㢖 䞮⮮㦮 㞫⩻゚㠦Ⱒ 㦮㫊䞮⓪ ộ㦒⪲ 㞢⩺㪎 㧞㠊 ⏎㯦⳿ ㌗⮮ 㺪⻚ 䡫㌗㦮 㡗䟻㦖 㦢㏣/㽞㦢

㏣ 㓺㤪㩲䔎㦮 ῂ㫆⯒ ἆ㩫䞮⓪ 㭒㣪 ⼖㑮⪲ ἶ⩺

♮㰖 㞠ἶ 㧞┺.

⽎ 㡆ῂ㠦㍲⓪ 㦢㏣/㽞㦢㏣ 㓺㤪㩲䔎 㥶☯㦮 Ὃ   㺪⻚ 䡫㌗㧊 㿿ỿ䕢 ῂ㫆 ⹥ 㞫⩻⿚䙂㠦 ⹎䂮

⓪ 㡗䟻㦚 㔺䠮㦚 䐋䞮㡂 㫆㌂䞮㡖㦒Ⳇ, ⏎㯦 Ὃ   㺪⻚䡫㌗㧊 㽞㦢㏣ 㓺㤪㩲䔎 ῂ㫆㠦 䋆 㡗䟻㦚

⹎䂾㦚 䢫㧎䞮㡖┺. 㔺䠮㠦㍲ ⏎㯦 㺪⻚ 䡫㌗㦮

⼖䢪⯒ 㥚䟊 㩲ỆṖ Ṗ⓻䞲 䝢⩂⁎㢖 㓺㤪㥶☯㦚 㥚䞲 4 Ṳ㦮 㥶㧛ῂ⪲ ῂ㎇♲ ⏎㯦㦚 㧊㣿䞲 㡂⩂

Ṗ㰖 䡫䌲㦮 㺪⻚ 䡫㌗㧊 ㌂㣿♮㠞┺. ⏎㯦 㞫⩻

゚⓪ 3.0 㠦㍲ 7.0 ₢㰖 ⼖䢪㔲䆆㦒Ⳇ, 䞒䏶 㿿☢㞫

⩻ ⹥ 㩫㞫㦚 䁷㩫䞮ἶ ㌺☚㤆⻫㦚 ㌂㣿䞮㡂 㥶☯

㧻㦚 Ṗ㔲䢪䞮㡖┺.

2 柪竞 沫獞 愕 愯憛

2.1 柪竞 沫獞

⽎ 㡆ῂ㠦㍲⓪ Fig.1 㠦 ⋮䌖⌎ ⹪㢖 ṯ㧊 㞫㿫

₆, 㩫㼊㔺, 䝢⩒ 㺪⻚, 䞒䏶 䝚⪲ぢ, Ἒ䁷 㔲㓺䎲

⹥ Ṗ㔲䢪 㔲㓺䎲㦒⪲ ῂ㎇♲ 㔺䠮 㧻䂮⯒ ㌂㣿䞮 㡖┺. 㞫㿫䍇䋂(3.0m 3 )㠦 㩖㧻♲ 㞫㿫Ὃ₆Ṗ ⏎㯦

㌗⮮㠦 㡆ἆ♲ 㩧㍶⹿䟻 㥶㧛ῂ⯒ Ṗ㰖⓪ 䝢⩒㺪

⻚㠦 Ὃ ♮Ⳇ, 䝢⩂⁎Ṗ 䝢⩒ 㺪⻚ 䡫㌗㦚 ⹪∎

₆ 㥚䟊 ㌂㣿♮㠞┺. Fig.2 㠦 ⽎ 㡆ῂ㠦㍲ ㌂㣿♲

⏎㯦ὒ 䝢⩂⁎ 䡫㌗㦚 ㌗㎎䞮Ợ ⋮䌖⌊㠞┺. ⏎㯦 㦖 ⳿₎㧊Ṗ 10mm 㧊Ⳇ, 㿲ῂ㰗ἓ De=8.0mm 㧎 㦢㏣ ⏎㯦㧊 ㌂㣿♮㠞┺. 㓺㤪㥶☯㦖 4 Ṳ㦮 㩧㍶

⹿䟻 㥶㧛ῂ㠦 㦮䟊 ⹲㌳䞮Ⳇ, ⏎㯦 Ὃ  㺪⻚㦮 䡫㌗㦚 ⼖䢪㔲䋺₆ 㥚䞮㡂 ⁎Ⱂ㠦㍲㢖 ṯ㦖 9 Ṳ 㦮 ㍲⪲ ┺⯎ 䡫㌗㦮 䝢⩂⁎Ṗ ㌂㣿♮㠞┺.

2.1 柪竞 浶兺刂 猧洛 愯憛

Computer

Light Source

Nozzle Plane Mirror

Concave Mirror

CCD Camera Pressure

Transducer

Pitot Tube Pin Hole

Traverse Pressure Transducer Ball Valve

Control Valve Compressor

Air Drier

Reservoir 1.4 Mpa 3 m3

Flow Meter Plenum

Chamber

Knife Edge Concave Mirror Plane Mirror

Flow

Amplifier

Hose

㪇㪈

Fig. 1 Schematic outlook of experimental facility.

Tangential flow Plug

Tangential flow

Dp=20

㱢

48 3

De=8

Supply chamber

10

x r

㩿㪬㫅㫀㫋㪑㩷㫄㫄㪀

Cf S2

30

S1-L

30 6

F0

30

26

C0 Cv

10

C10

10

C30

300

12

S1-S

6

6.2

10

To atm.

55

5

I I I I

Fig. 2 Details of supply chamber, nozzle, and plug configurations (Unit : mm).

(3)

㓺㤪 㥶☯㠦 ╖䞮㡂, ₆䞮䞯㩗 㓺㤪㑮(Sg)⓪ ┺㦢 ὒ ṯ㦖 㓺㤪ṫ☚⪲ 㩫㦮♲┺ (12) .

¿ ¾

½

¯ ®

­

 m ) m ( ) m A / D r ( S

a t

e p

g  



T

S 2 T (1)

m pm s ⓪ ṗṗ 㿫⹿䟻 ⹥ 㩧㍶⹿䟻 㥶㧛ῂ⯒

䐋䞮⓪ 㰞⨟㥶⨟㧊┺. r

p

, D

e

, A

t

(㥶㧛ῂ㩚㼊Ⳋ㩗)⓪ Fig.2 㠦 ⋮䌖⌊㠞┺. 㔺䠮㠦㍲ m T ⹥ m a ⓪ ⏎㯦

㌗⮮ 㥶㧛ῂ㠦 ㍺䂮♲ ⻺䓲ⰂⲪ䌖⯒ 䐋䟊 䁷㩫♮

㠞┺. Eq. (1)㠦 㦮䟊 㩫㦮♲ ₆䞮䞯㩗 㓺㤪㑮⓪ 㿲 ῂ㏣☚ ⿚䙂⯒ ἶ⩺䞮㰖⓪ 㞠㞮┺. ⽎ 㡆ῂ㠦㍲⓪ 㩧㍶⹿䟻㦮 㥶☯Ⱒ 㧞⓪ ἓ㤆⪲ ⏎㯦䡫㌗㠦 㦮䟊

㍲Ⱒ ἆ㩫♮Ⳇ 㓺㤪㑮 Sg=0.81 ⪲ ἶ㩫♮㠞㦒Ⳇ,

⏎㯦㧛ῂ㦮 ㌗⮮ 㩫㼊㞫(P

01

)ὒ 㿲ῂ㦮 ╖₆㞫(P

a

) 㠦 ╖䞲 㞫⩻゚(NPR)⯒ 3.0~7.0 ₢㰖 ⼖䢪㔲䆆┺.

㣎ἓ㧊 0.8mm, ⌊ἓ㧊 0.5mm 㧎 䞒䏶 䝚⪲ぢṖ 㽞㦢㏣ 㓺㤪㩲䔎 㥶☯㧻㦮 㿫⹿䟻 ⹥ ⹮ἓ⹿䟻㦒

⪲㦮 㿿☢ 㞫⩻㦚 䁷㩫䞮₆ 㥚䟊 ㌂㣿♮㠞┺.

3. 冶刂 愕 処然

Fig.3 㦖 F0 ἓ㤆㠦 ╖䞲 ╖䞲 Ṗ㔲䢪 ㌂㰚ὒ ⏎㯦 㭧㕂㿫 ⿖⁒㠦㍲㦮 㿿☢㞫⩻ ⿚䙂⯒ ⋮䌖⌊Ⳇ, ⏎ 㯦 㞫⩻゚⓪ 3.0~7.0 ₢㰖 ⼖䢪䞲┺. 㧒⹮㩗㦒⪲

㓺㤪㥶☯㠦㍲ 㓺㤪 ṫ☚Ṗ 㧒㩫Ṩ 㧊㌗㧊 ♮Ⳋ 㥶

☯㧻 ⌊㠦 㡃⮮㡗㡃, 㯟, ⏎㯦 㭧㕂㿫⿖⁒㠦㍲㦮 㡃㞫⩻ῂ⺆ 㡗㡃㧊 㫊㨂䞮Ợ ♲┺. ⽎ 㡆ῂ㠦㍲☚

NPR=3.0 㧎ἓ㤆 㩲䔎⓪ 㟓Ṛ ⿖㫇 䖓㺓㧊 ♮Ⳇ ⏎ 㯦 㿲ῂ㠦 ἓ㌂ 㿿ỿ䕢Ṗ 䡫㎇♲┺. ⁎⩂⋮ ἓ㌂

㿿ỿ䕢⓪ ゚㓺㤪 㥶☯㧎 ἓ㤆㠦㍲㢖 ṯ㧊 ⏎㯦 㭧 㕂㿫㠦㍲ ⹮㌂䞮㰖 㞠ἶ, 㩲䔎 㭧㕂⿖㠦 ⹲㌳䞲 㨂㑲䢮 㡗㡃㦮 ἓἚ㠦㍲ ⹮㌂䞮⓪ ộ㦚 ⽒ 㑮 㧞

┺. NPR ⯒ ▪㤇 㯳Ṗ㔲䌊㠦 ➆⧒ 㩲䔎 㥶☯㦖 ⏎ 㯦 㿲ῂ㠦㍲ ▪㤇 䋂Ợ ⿖㫇䖓㺓 ♮Ⳇ ⹪⩦ 㿿ỿ 䕢(barrel shock wave)⯒ ⽒ 㑮 㧞ἶ 㥶☯㧻㦖 㽞㦢

㏣ 㥶☯㡗㡃ὒ 㓺㤪 㥶☯㦒⪲ 㧎䞲 㨂㑲䢮 㡗㡃㦒

⪲ ⿚Ⰲ♾㦚 ⳛ䢫䧞 㞢 㑮 㧞┺. 㧊⓪ Yu &

Chen (12) 㦮 㡆ῂ㠦㍲☚ 䢫㧎 䞲 ⹪ 㧞┺. NPR=7.0 㦒⪲ 㯳Ṗ䞮Ⳋ Fig. 3(b)㠦 ゚䟊 㨂㑲䢮 㡗㡃㦮 䋂

₆⓪ 㯳Ṗ䞮Ⳇ ⹪⩦㿿ỿ䕢⓪ ▪㤇 ṫ䟊㰖Ợ ♲┺.

⡦䞲 㨂㑲䢮 㡗㡃㦮 㾲╖ 㰗ἓ㦖 㞫⩻゚㠦 ➆⧒

㯳Ṗ䞮ἶ ╖⨋㩗㦒⪲ ┺㧊㞚ⴂ✲ 䡫㌗㦚 ⋮䌖⌊ἶ 㧞┺. 㧊⩂䞲 㥶☯䔏㎇㦖 㿿☢㞫⩻⿚䙂㠦㍲ 㫖▪

㩫⨟㩗㦒⪲ 䢫㧎 䞶㑮 㧞┺. 㩗㣿♲ ⳾✶ 㞫⩻゚

㠦 ╖䞮㡂 ⏎㯦 㿲ῂ㠦㍲ 㿿☢㞫⩻㦖 㦢(negative) 㦮 Ṩ㦚 Ṗ㰖Ⳇ 㧊⓪ 㧊 㡗㡃㦮 㥶☯㧊 㡃⮮䞾㦚

(a) p

01

/p

a

= 3.0

(b) p

01

/p

a

= 5.0

(c) p

01

/p

a

= 7.0

p imp ac t /p 01 (G ag e)

x/D e

p

01

/p

a

= 3.0 p

01

/p

a

= 5.0 p

01

/p

a

= 7.0

0 2 4 6 8 10

-0.4 -0.2 0 0.2 0.4

Fig.3 Shadowgraph pictures and impact pressure distributions(F0)

㦮⹎䞲┺. NPR 㧊 㯳Ṗ䞾㠦 ➆⧒ 㡃⮮㡗㡃㦖 Ṧ㏢

䞮Ợ ♮Ⳇ, 䘟‶㿿☢㞫⩻㦖 㯳Ṗ䞮ἶ 㧞㠊 ⿖㫇䖓 㺓 㓺㤪㩲䔎 ῂ㫆⓪ ⏎㯦 㞫⩻゚㠦 䋂Ợ 㡗䟻㦚

⹱⓪┺⓪ ộ㦚 㞢 㑮 㧞┺. 㨂㑲䢮 㡗㡃⌊㠦㍲ 㿿

☢㞫⩻⿚䙂㦮 㯳Ṗ㢖 Ṧ㏢⓪ 㓺㤪㩲䔎⌊㠦 ⹲㌳䞮

⓪ 㿿ỿ䕢㦮 㨂㑲䢮 㡗㡃ἓἚ㠦㍲ 㧛㌂ ⹥ ⹮㌂㠦

➆⯎ 㡗䟻㧊⧒ ㌳ṗ♮㠊 㰚┺.

3.1 煚憊 啣埮抆 笛旇汞 欇窫

-0.4 -0.2 0 0.2

-0.4 -0.2 0

p /p imp ac t 01 (G ag e) 0.2

x/D e

( F0, C0, Cv ) p

01

/p

a

= 3.0

p

01

/p

a

= 5.0

p

01

/p

a

=7 .0

0 1 2 3 4 5 6 7 8 9 10

-0.4 -0.2 0 0.2

Fig.4 Impact pressure distributions

Fig.4 㠦⓪ 㺪⻚ ⊳┾⿖ 䡫㌗㧊 㿿☢㞫⩻ ⿚䙂㠦

⹎䂮⓪ 㡗䟻㦚 ゚ᾦ䞮㡖┺. ⊳┾⿖㦮 䡫㌗㧊 䘟Ⳋ (F0), 㡺⳿(C0) ⹥ ⽒⪳(Cv) 䡫䌲㦮 䝢⩂⁎Ṗ ㌂㣿

♮㠞㦒Ⳇ NPR=3.0~7.0 ₢㰖 ⼖䢪䞲┺. NPR=3.0 㧎

(4)

ἓ㤆, F0 ἓ㤆Ṗ C0 㢖 Cv ⽊┺ 䘟‶㿿☢㞫⩻㧊 ⌄ ἶ, C0 㢖 Cv ἓ㤆⓪ Ệ㦮 㥶㌂䞲 㿿☢ 㞫⩻⿚䙂 Ṩ㦚 ⽊㡂㭒ἶ 㧞┺. ⁎⩂⋮ 㧊⩂䞲 㹾㧊☚ NPR Ṗ 㯳Ṗ䞾㠦 ➆⧒ 㩦㹾 Ṧ㏢䞮ἶ 㧞㦒Ⳇ 㩗㣿♲

⳾✶ ἓ㤆㠦 ╖䞮㡂 ☯㧒䞲 ⿚䙂ἓ䟻㦚 ⽊㡂㭒ἶ 㧞㠊 㺪⻚ ⊳┾⿖㦮 䡫㌗㦖 ⿖㫇䖓㺓 㓺㤪 㩲䔎䔏

㎇㠦 䋆 㡗䟻㦚 ⹎䂮㰖 㞠⓪┺ἶ ㌳ṗ♮㠊 㰚┺.

3.2 洛橛击 (Pressure tap )汞 欇窫

(Cf) (C30) (C10) (C0)

-0.4 -0.2 0 0.2 0.4

-0.4 -0.2 0 0.2

p /p im pa ct 01(Ga ge ) 0.4

x/D e

( C0, C10, C30, Cf )

p

01

/p

a

= 7.0 p

01

/p

a

= 5.0 p

01

/p

a

= 3.0

0 1 2 3 4 5 6 7 8 9 10

-0.4 -0.2 0 0.2 0.4

p

01

/p

a

= 7.0

Fig.5 Shadowgraph pictures and impact pressure distributions

㞴㠦㍲☚ ㍲㑶䞮㡖❅㧊, 㧒⹮㩗㦒⪲ ⏎㯦㦚 㧊㣿 䞲 㡆ῂ㠦㍲⓪ ⏎㯦㌗⮮㦮 㩫㼊㩦 㞫⩻㦚 䁷㩫䞮

₆ 㥚䞮㡂 㰗ἓ 1mm-10mm 㩫☚㦮 㩫㞫Ὃ㦚 㧊㣿 䞮ἶ 㧞┺.

㧊⩂䞲 㩫㞫Ὃ㧊 㓺㤪 㩲䔎㠦 ⹎䂮⓪ 㡗䟻㦚 䢫㧎 䞮₆ 㥚䞮㡂 㺪⻚ ⊳┾⿖㠦 㰗ἓ 5mm 㦮 㩫㞫Ὃ 㦚 ṖὋ䞮ἶ ⏎㯦⌊Ⳋ㠦㍲ 㞫⩻㎒㍲₢㰖㦮 ỆⰂ⯒

⼖䢪㔲䋺Ⳋ㍲ 㫆㌂䞲 ἆὒ⯒ Fig.5 㠦 ⋮䌖⌊㠞┺.

Ṗ㔲䢪 ㌂㰚㦚 ⽊Ⳋ, 䢖(㩫㞫Ὃ)㦮 ₠㧊(⏎㯦⌊Ⳋ 㠦㍲ ⿖䎆 㞫⩻㎒㍲ ⿖㹿㥚䂮₢㰖㦮 ỆⰂ)㠦 ➆⧒

㿿ỿ䕢 ῂ㫆⓪ 䋂Ợ ╂⧒ 㰖⓪ ộ㦚 㞢 㑮 㧞┺.

䔏䧞 C10 䝢⩂⁎Ṗ ㌂㣿♲ ἓ㤆 㩲䔎㥶☯⌊㠦 㨂 㑲䢮 㡗㡃㧊 ⽊㧊㰖 㞠ἶ ゚㓺㤪㩲䔎㠦㍲ ⹲㌳䞮

⓪ Ⱎ䞮❪㓺䋂Ṗ 䡫㎇♮ἶ 㧞㦢㦚 ⽒ 㑮 㧞┺.

C30 㦮 ἓ㤆☚ ⏎㯦㿲ῂ 㴓㦒⪲ Ⱒἷ♲ 㿿ỿ䕢Ṗ 䡫㎇♮ἶ 㧞㦒Ⳇ 㨂㑲䢮 㡗㡃㦮 ῂ㫆⓪ C0 ἓ㤆㠦

゚䟊 䋂Ợ ┺⯎ 䡫㌗㦚 ⽊㡂㭒ἶ 㧞┺. 㧊⩂䞲 㩫 㞫Ὃ㧊 ⿖㫇䖓㺓 㓺㤪㩲䔎 䔏㎇㠦 ⹎䂮⓪ ἓ䟻㦖 㿿☢ 㞫⩻⿚䙂㠦㍲ 㫖▪ ⳛ䢫䧞 㞢㑮 㧞┺.

NPR=3.0 㧎 ἓ㤆㠦 㿿☢㞫⩻⿚䙂⓪ 㩫㞫Ὃ ₠㧊㠦

➆⧒ 䋆 㹾㧊⯒ ⽊㧊⋮ 㩗㣿♲ ⳾✶ ἓ㤆㠦 㦢

(negative)㦮 㿿☢㞫⩻ Ṩ㦚 ⋮䌖⌊ἶ 㧞㠊 㨂㑲䢮 㡗㡃㧊 㫊㨂䞾㦚 㞢 㑮 㧞┺. 䘟‶ 㿿☢㞫 ⿚䙂

⓪ C10 ἓ㤆Ṗ ἓ㤆Ṗ Ṗ㧻 ⏨㦒Ⳇ, C0 ἓ㤆Ṗ Ṗ 㧻 ⌄Ợ ⋮䌖⋮ἶ, ⏎㯦 㞫⩻゚Ṗ 㯳Ṗ䞶㑮⪳ ⁎ 㹾㧊⓪ 㩦㹾 Ṧ㏢䞮ἶ 㧞┺. NPR=5.0, 7.0 㧎 ἓ㤆, C10 㦮 ἓ㤆⓪ 䝢⩂㓺 㿿☢㞫⩻Ṩ㦚 ⋮䌖⌊ἶ 㧞 㠊 㨂㑲䢮 㡗㡃㧊 㠜㦢㦚 㞢 㑮 㧞┺. 㧊⩂䞲 ⏎ 㯦 㞫⩻゚㠦 ➆⯎ 㡗䟻㦖 ⏎㯦 㞫⩻゚㠦 ➆⧒ ⹲

㌳♮⓪ ㍶䣢⮮ ⹥ 㿿ỿ䕢 ṫ☚㠦 ὖ⩾㧊 㧞┺ἶ

㌳ṗ♮㠊 㰚┺.

3.3 旃沋夢 毖皻笛 戏汞 欇窫

( S2 ) ( S1-L )

( F0 )

(a) p 01 /p a = 3.0 (b) p 01 /p a = 7.0 Fig.6 Shadowgraph pictures

Fig.6 㠦⓪ F0 ἓ㤆⯒ ₆㭖㦒⪲ ⏎㯦 Ὃ  㺪⻚

⌊㠦 㙦₆ 䡫㌗(S1-L) ⹥ ⽒䔎 䡫㌗(S2)㦮 ⽟㦚 㧊 㣿䞮㡂 ⏎㯦 ⌊⿖㠦 ㍺䂮♮⓪ 㡊㩚╖㦮 㡗䟻㦚 㫆

㌂䞮₆ 㥚䞲 Ṗ㔲䢪 ㌂㰚㦚 ⋮䌖⌊㠞┺. S1-1 ⹥ S2 㦮 䡫㌗㦖 Fig.2 㠦 㧦㎎䧞 ⋮䌖⌊㠞┺. NPR=3.0 㧎 ἓ㤆, ⳾✶ ἓ㤆㠦 ╖䞮㡂 㥶☯㧻㦖 䋆 ⼖䢪Ṗ 㠜⓪ ộ㦒⪲ ⽊㡂㰚┺. ⁎⩂⋮ NPR Ṗ 7.0 㦒⪲ 㯳 Ṗ䞲 ἓ㤆, ⽟㦮 㫊㨂 ⹥ 䡫㌗㠦 ➆⧒ 㓺㤪㩲䔎 ῂ㫆⓪ ┺⯊ἶ S1-L 㦮 ἓ㤆, C10 ἓ㤆㢖 Ⱎ㺂Ṗ㰖

⪲ 㨂㑲䢮 㡗㡃㦖 ⽊㧊㰖 㞠㦒Ⳇ ṫ䞲 Ⱎ䞮❪㓺䋂 Ṗ 䡫㎇♮ἶ 㧞㦢㦚 㞢 㑮 㧞┺.

㧊ộ㦚 㩫⨟㩗㦒⪲ 㫆㌂䞮₆ 㥚䞮㡂 ṗṗ㦮 ἓ㤆 㠦 ╖䞲 㿫⹿䟻 ⹥ ⹮ἓ⹿䟻㦒⪲㦮 㿿☢ 㞫⩻⿚䙂

⯒ Fig.7 ⹥ Fig.8 㠦 ⋮䌖⌊㠞┺. S1-L ἓ㤆 ⳾✶ 㞫

⩻゚㠦㍲ 㦢(negative)㦮 㿿☢㞫⩻Ṩ㦖 ⋮䌖⋮㰖 㞠㦒Ⳇ 㧒⹮㩗㧎 㽞㦢㏣ ゚㓺㤪 㩲䔎㢖 ⰺ㤆 㥶㌂

䞲 ἓ䟻㦚 ⽊㧊ἶ㧞┺ (13) . ⹮Ⳋ㠦 S2 ἓ㤆 F0 ἓ㤆

(5)

-0.4 -0.2 0 0.2 0.4

-0.4 -0.2 0 0.2

p /p

impact01(Gage)

0.4

x/D

e

( F0, S1-L, S2 )

p01

/p

a

= 7.0

p01

/p

a

= 5.0

p01

/p

a

= 3.0

0 1 2 3 4 5 6 7 8 9 10

-0.4 -0.2 0 0.2 0.4

Fig.7 Impact pressure distributions

= 1 . 0

0 1 . 0

r/De

pi m p a c t/ p0 1 ( G a g e ) x / De= 0 . 1

( b ) p0 1/ pa = 7 . 0

0 1 . 0

- 1 - 0 . 5 0 0 . 5

1 = 2 . 0

0 1 . 0

= 3 . 0

0 1 . 0

= 1 1 . 0

0 1 . 0

= 1 . 0

0 1 . 0

r/De

pi m p a c t/ p0 1 ( G a g e ) x / De= 0 . 1

( F 0 , S 1 - L , S 2 )

( a ) p0 1/ pa = 3 . 0

0 1 . 0

- 1 - 0 . 5 0 0 . 5

1 = 2 . 0

0 1 . 0

= 3 . 0

0 1 . 0

= 1 1 . 0

0 1 . 0

Fig.8 Radial impact pressure distributions

⽊┺ 䘟‶ 㿿☢㞫⩻㧊 ⏨Ợ ⋮䌖⋮Ⳇ 㨂㑲䢮 㡗㡃 㧊 㫊㨂䞮⓪ ộ㦚 㞢㑮 㧞┺. 䔏㧊䞲 ộ㦖 S2 ἓ 㤆, NPR 㧊 㯳Ṗ䞮Ⳋ ⏎㯦 㿲ῂ㠦㍲⓪ 䝢⩂㓺 㿿

☢㞫⩻Ṩ㦚 Ṗ㰖ἶ 㫆⁞ 䞮⮮㠦㍲ 㦢(negative)㦮 㿿☢ 㞫⩻Ṩ㦚 Ṗ㰖ἶ 㧞㠊 Ὃ 㺪⻚ 䡫㌗㧊 㨂㑲 䢮 㡗㡃㦮 ⹲㌳㥚䂮 ⹥ 䡫㌗㠦 㡗䟻㧊 㧞㦢㦚 㞢 㑮 㧞┺. 㨂㑲䢮 㡗㡃㦮 㰗ἓ ⹥ 㨂㑲䢮 ṫ☚ 䔏

㎇㦖, ⹮ἓ⹿䟻 㿿☢㞫⩻, ⁎Ⱂ 8 㠦㍲ 㞢 㑮 㧞┺.

⁎Ⱂ㦮 䣷㿫㦖 ⏎㯦 㭧㕂㠦㍲㦮 㿿☢㞫⩻㦚, 㫛㿫 㦖 ⏎㯦㭧㕂㿫㠦㍲ ⹮ἓ⹿䟻㦒⪲㦮 ỆⰂ⯒ ⏎㯦 㿲ῂ 㰗ἓ D ⪲ ⶊ㹾㤦 䞲 ỆⰂ⯒ ⋮䌖⌊ἶ 㧞┺.

䁷㩫♲ ⏎㯦 㿿☢㞫⩻㧊 㦢(negative)㦮 Ṩ㦚 Ṗ㰖

⓪ 㡗㡃㧊 㥶☯㧊 㨂㑲䢮 ♮⓪ 㡗㡃㦒⪲, 㧊 㡗㡃 㠦㍲㦮 r/De Ṩ㦖 㨂㑲䢮 㡗㡃㦮 ⹮ἓ㦚 㦮⹎䞲┺.

NPR=3.0 㧎 ἓ㤆, S1-L ἓ㤆⓪ 㞴㠦㍲☚ ㍲㑶䞲ộ ὒ ṯ㧊 㨂㑲䢮 㡗㡃㦚 Ṗ㰖ἶ 㧞㰖 㞠㦒⋮, F0

⹥ S2 ἓ㤆⓪ 㨂㑲䢮 㡗㡃㧊 ⋮䌖⋮ἶ 㧞┺. ⁎⩂

⋮ S2 ἓ㤆⓪ ⏎㯦 䞮⮮㴓㦒⪲ 㰚䟟䞮Ⳋ㍲  ㏣㧊 Ṧ㏢䞮㡂 x/De=2.0 㠦㍲⓪ 㨂㑲䢮㦖 㫛⬢♮ἶ 㧞㦒

⋮, F0 ἓ㤆⓪ 䞮⮮⪲ 㰚䟟䞮Ⳋ㍲ 㨂㑲䢮 㡗㡃 㰗

ἓ㦖 ▪㤇 㯳Ṗ䞮ἶ 䞮ἶ 㧞㦢㦚 㞢㑮 㧞┺.

NPR=7.0 㧎 ἓ㤆 㨂㑲䢮 㡗㡃㦮 㰗ἓ㦖 NPR=3.0 㦮 ἓ㤆㠦 ゚䞮㡂 䤾㞂 䋂⋮ 㡃 㞫⩻ῂ⺆⓪ 㧧㦖 ộ㦒⪲ ⽊㡂 㰚┺. ⏎㯦 Ὃ  㺫⻚ ⌊㠦 ㌓㧛♮⓪

⽟㦖(㡊㩚╖) 㓺㤪 㩲䔎ῂ㫆 䔏䧞 㨂㑲䢮 㡗㡃㦮

㌂㧊㯞, 㥚䂮 ⹥ 㨂㑲䢮 ṫ☚㠦 䋂Ợ 㡗䟻㦚 ⹎䂾 㦚 㞢㑮 㧞┺.

3.4 旃沋夢 毖皻笛 戏汞 氊獞櫖 娶幾 欇窫

-0.4 -0.2 0 0.2 0.4

-0.4 -0.2 0 0.2

p /p im pact 01 (G ag e) 0.4

x/D e

( F0, S1-S, S1-M, S1-L)

p

01

/p

a

= 5.0

p

01

/p

a

= 7.0 p

01

/p

a

= 3.0

0 1 2 3 4 5 6 7 8 9 10

-0.4 -0.2 0 0.2 0.4

Fig.9 Impact pressure distributions

Fig.9 ⓪ 㺪⻚㠦 ㌓㧛♲ 㤦䐋䡫 ⽟㦮 㥚䂮㠦 ➆

⯎ 㿿☢㞫⩻ ⿚䙂 䔏㎇㦚 ⋮䌖 ⌎ ộ㧊┺. S1-L 㦮 ἓ㤆⓪ 㤦䐋 ⊳┾⿖Ṗ 㩧㍶⹿䟻 㥶㧛ῂ㠦 㥚䂮 䞮Ⳇ, S1-M ὒ S1-L ἓ㤆⓪ 㩧㍶⹿䟻 㥶㧛ῂ⽊┺

䞮⮮㠦 㥚䂮䞲┺. NPRp=3.0 㠦㍲ S1-M ὒ S1-L ἓ 㤆⓪ 㨂㑲䢮 㡗㡃㦚 Ṗ㰖㰖 㞠⓪ ộ㦒⪲ ⋮䌖⋮ἶ 㞫⩻゚ ⹥ ⽟㦮 㥚䂮㠦 ➆⧒ 㓺㤪 㩲䔎ῂ㫆Ṗ 䋆 㡗䟻㦚 ⹱⓪┺⓪ ộ㦚 㞢 㑮 㧞┺.

3.5 筂穯 匾決櫖 惾獞垚 欇窫

Fig. 10 㦖 㽞㦢㏣ 㡗㡃ὒ 㡃⮮ 㡗㡃㦒⪲ ⋮⒮㠊㰚 㽞㦢㏣ 㓺㤪㥶☯㧻㧊 㿿⿚䞲 䢒䞿㧊 㧊⬾㠊㪎 㧒 㩫䞲 㞫⩻ ┾Ⳋ㦚 Ṗ㰖⓪ 㥚䂮₢㰖㦮 ⏎㯦 㿲ῂ⪲

⿖䎆㦮 ỆⰂ⯒ 䢒䞿₎㧊⪲ 㩫㦮䞮㡂 ⏎㯦 㿲ῂ 㰗 ἓ D ⪲ ⶊ㹾㤦 䞲 Ṩ㦚 ⋮䌖⌎ ộ 㧊┺. ⁎Ⱂ㠦

㍲ 㞢 㑮 㧞❅㧊 㞫⩻゚Ṗ 㯳Ṗ䞶㑮⪳ 䢒䞿₎㧊⓪ 㯳Ṗ䞮ἶ ⏎㯦 㺪⻚ 䡫㌗㠦 㡗䟻㦚 ⹱⓪ộ㦚 㞢㑮 㧞┺. S1-L ἓ㤆, F0 㠦 ゚䞮㡂 㾲╖ 㟓 42%, 㾲㏢

㟓 13% Ṧ㏢䞮ἶ 㧞┺. 㧊⩂䞲 䢒䞿㡗㡃㦮

(6)

o-a : 1 mm o-b : 3 mm

Nozzle

o ab

㱢 8

x m /D e p

i0

/p

01

x/D e

o a b

F0 C30 S1-L S2

x m /D e

p 01 /p a

3 4 5 6 7

4 5 6 7 8 9 10 11 12

Fig.10 Mixing length of the swirling flow

㥚䂮⓪ 㡆㏢㠦㍲ ⹲㌳䞮⓪ 䢪㡒㦮 ₎㧊 ⹥ 㞞㩫䢪 㠦 㭧㣪䞲 ⼖㑮⪲ 㧧㣿䞮Ⳇ, ⏎㯦 㺪⻚䡫㌗㦚 㧊 㣿䞮㡂 㫆㩞㧊 Ṗ⓻䞮┺⓪ ộ㦚 ⽊㡂 㭒ἶ 㧞┺.

4 冶 嵦

⽎ 㡆ῂ⓪ ⏎㯦 Ὃ  㺪⻚ 䡫㌗㧊 ⿖㫇䖓㺓 㓺 㤪㩲䔎 ῂ㫆㠦 ⹎䂮⓪ 㡗䟻㦚 㔺䠮㦚 䐋䞮㡂 㫆㌂

䞮㡖┺. 㧊⯒ 㥚䞮㡂 ⏎㯦 㞫⩻゚ ⹥ 㺪⻚ 䡫㌗㦚

⼖䢪㔲䋺Ⳋ㍲ 㓞Ⰲ⩢ ὧ䞯⻫㦚 ㌂㣿䞮㡂 㥶☯㧻㦚 Ṗ㔲䢪䞮㡖ἶ, 㿿☢㞫⩻ ⿚䙂⯒ 䁷㩫䞮㡖┺. ⁎ ἆ ὒ, ⏎㯦 㺪⻚ 䡫㌗㦖 ⿖㫇䖓㺓 㓺㤪㩲䔎㦮 㭒㣪 䔏㎇, 㯟 㩲䔎㥶☯㧻 㿿☢ 㞫⩻⿚䙂, 㨂㑲䢮 㡗㡃 ỆⰂ ⹥ 㰗ἓ, ⁎Ⰲἶ 䢒䞿ỆⰂ❇㠦 䋆 㡗䟻㦚 ⹎ 䂮⓪ ộ㦚 㞢 㑮 㧞㠞┺. 㽞㦢㏣ ⏎㯦 ⹥ 㩧㍶ ⹿ 䟻㦮 㓺㤪 㥶☯㦚 㧊㣿䞲 㽞㦢㏣ 㓺㤪 㩲䔎䔏㎇

㡆ῂ㠦㍲⓪ ⏎㯦⌊ 㡊㩚╖ ⹥ 㩫㞫Ὃ ㍺䂮㠦 䔏

⼚䞲 㭒㦮⯒ 䟊㟒䞮Ⳇ, ⏎㯦 㺪⻚ 䡫㌗㦚 㧊㣿䞮 㡂 㨂㑲䢮 㡗㡃㦮 ㌂㧊㯞⯒ 䄾䔎⪺ 䞶 㑮 㧞㦢㦚 䢫㧎 䞮㡖┺. ⁎⩂⋮ 㞴㦒⪲ ⏎㯦 㺪⻚ 䡫㌗㧊 㓺 㤪 㥶☯䔏㎇㠦 ⹎䂮⓪ Ⲫ䃊┞㯮㠦 ╖䞲 ㌗㎎䞲 㡆 ῂṖ 䞚㣪䞮┺.

焾処怾竒

(1) Lilley D.G., 1977, “Swirl Flows in Combustion: A Review,” AIAA Journal, Vol. 15, No. 8, pp. 1063-1078.

(2) Mauchton J. W., Cattafesta III L.N., and Settles G.S., 1996, “An experimental study of compressible turbulent mixing enhancement in swirling jets,” J.

Fluid Mech., Vol. 330., pp.271-305.

(3) Syred, N. and Beer, J. M., 1974, “Combustion in swirling floes,” Combustion and Flame, Vol. 23, pp.

143-201.

(4) Yu Y.K., Chen R.H, and Chew L., 1998, “A Screech Tone Noise and Mode Switching in Supersonic Swirling Jets,” AIAA Journal, Vol. 36, No. 11, pp.1968-1974.

(5) Rose W.G., 1962, “Swirling Round Turbulent Jet,”

Journal of Applied Mechanics, Vol. 29, pp. 616-625.

(6) Chigier N.A. and Beer J.M., 1964, “Velocity and Static Pressure distributions in Swirling Air Jets Issuing from Annular and Divergent Nozzles,” Journal of Basic Engineering, Vol. 86, pp. 788-798.

(7) Kerr N.M. and Fraser D., 1965, “Swirl. Part 1 : Effect on Axisymmetrical Turbulent Jets,: Journal of the Institute of Fuel, Vol. 38, No. 299, pp. 519-526.

(8) Carpenter P.W. and Johannesen N.H., 1974, “An Extension of One-Dimensional Theory to Inviscid Swirling Flow through Chocked Nozzles,”

Aeronautical Quarterly, pp. 71- 87.

(9) Carpenter P.W., 1985, “A Linearized Theory for Swirling Supersonic Jets and Its Application to Shock- Cell Noise. AIAA Journal. Vol. 23, No. 12, pp. 1902- 1909.

(10) Dutton J.C., 1987, “Swirling Supersonic Nozzle Flow,” J. Propulsion, Vol. 3, pp.342-349.

(11) Culter A. D., Levey B.S., and Kraus D.K., 1995,

“Near-Field Flow of Supersonic Swirling Jets,” AIAA Journal, Vol. 33, No. 5, pp. 876-881.

(12) Yu Y.K and Chen R.H., 1997, “A Study of Screech Tone Noise of Supersonic Swirling Jets,” Journal of Sound and Vibration, Vol.205, No.5, pp 698-705.

(13) Katanoda H., Miyajato Y., Masuda M., and Matsuo

K., 2000, “Pitot Pressure of Correctly-Expended and

Underexpanded Free Jets form Axisymmetric

Supersonic Nozzles,” Shock Waves, Vol. 10, pp. 95-

101.

수치

Fig. 1 Schematic outlook of experimental facility.

참조

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