⏎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
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
㫇
㪇㪈Fig. 1 Schematic outlook of experimental facility.
Tangential flow Plug
Tangential flow
Dp=㱢20
㱢
48 3
De=㱢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).
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 p m 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
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
-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