JPH0453559Y2 - - Google Patents

Info

Publication number
JPH0453559Y2
JPH0453559Y2 JP4124386U JP4124386U JPH0453559Y2 JP H0453559 Y2 JPH0453559 Y2 JP H0453559Y2 JP 4124386 U JP4124386 U JP 4124386U JP 4124386 U JP4124386 U JP 4124386U JP H0453559 Y2 JPH0453559 Y2 JP H0453559Y2
Authority
JP
Japan
Prior art keywords
pressure side
diaphragm
low
supersonic
blade
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired
Application number
JP4124386U
Other languages
English (en)
Japanese (ja)
Other versions
JPS62153552U (show.php
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed filed Critical
Priority to JP4124386U priority Critical patent/JPH0453559Y2/ja
Publication of JPS62153552U publication Critical patent/JPS62153552U/ja
Application granted granted Critical
Publication of JPH0453559Y2 publication Critical patent/JPH0453559Y2/ja
Expired legal-status Critical Current

Links

Landscapes

  • Aerodynamic Tests, Hydrodynamic Tests, Wind Tunnels, And Water Tanks (AREA)
  • Testing Of Engines (AREA)
JP4124386U 1986-03-20 1986-03-20 Expired JPH0453559Y2 (show.php)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP4124386U JPH0453559Y2 (show.php) 1986-03-20 1986-03-20

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP4124386U JPH0453559Y2 (show.php) 1986-03-20 1986-03-20

Publications (2)

Publication Number Publication Date
JPS62153552U JPS62153552U (show.php) 1987-09-29
JPH0453559Y2 true JPH0453559Y2 (show.php) 1992-12-16

Family

ID=30856061

Family Applications (1)

Application Number Title Priority Date Filing Date
JP4124386U Expired JPH0453559Y2 (show.php) 1986-03-20 1986-03-20

Country Status (1)

Country Link
JP (1) JPH0453559Y2 (show.php)

Also Published As

Publication number Publication date
JPS62153552U (show.php) 1987-09-29

Similar Documents

Publication Publication Date Title
US4105364A (en) Vane for a gas turbine engine having means for impingement cooling thereof
JPS61144540A (ja) 温度プローブ
US2573834A (en) Duct intake or entry for gaseous fluid flow diffuser system
JP7421769B2 (ja) ダクト内圧力計測構造及び風洞試験装置
JPH0453559Y2 (show.php)
JP2007513282A (ja) ステータの表面流れを変えることによりターボエンジンの騒音を減少させる方法
JP5023213B2 (ja) 噴射騒音が軽減される航空機用ターボシャフト・エンジン
Liesner et al. Combination of active and passive flow control in a high speed compressor cascade
CN112682107B (zh) 带有穿孔肋的涡轮叶片尾缘冷却结构及方法和燃气轮机
US5407133A (en) Cooled thin metal liner
JP2515800B2 (ja) 環境風洞試験装置
CN110886666A (zh) 一种自适应气动力密封的二元可调喷管
JPS6139482B2 (show.php)
JP3353041B2 (ja) 超音速機のインテーク側壁
JPH09145534A (ja) 超音速ノズル
WO1997019257A1 (en) Vane for gas turbine
JPH072950U (ja) 吸込式衝撃風洞
GB791463A (en) Means inducing a flow of cooling air for internal combustion engines
Davidson Some properties of the compression shock as in turbine and compressor blade passages
Prabakar et al. Investigation of diffusers for two stream supersonic wind tunnels
US3832903A (en) Stagnation pressure probe
Liang Cooled thin metal liner
Lepicovsky Effects of Transducer Installation on Unsteady Pressure Measurements on Oscillating Blades
Kobayashi Effect of Shock Wave Movement on Aerodynamic Instability of Annular Cascade Oscillating in Transonic Flow
JP2000292269A (ja) ターボ機械の流体温度計測装置