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The inlet

The inlet
紙図書
Claire Tham.Ethos Books[2013]<X>
国立国会図書館

Numerical study of backflow and backflow vortex at the inlet of inducers

Numerical study of backflow and backflow vortex at the inlet of inducers
紙博士論文
Xiangyu Qiao [著][Xiangyu Qiao]2005<UT51-2006-C210>
国立国会図書館

Investigation of acoustic phenomena at the inlet and the outlet of a centrifugal compressor for pressure ratio 4.5 ASME-2001-GT-314

Investigation of acoustic phenomena at the inlet and the outlet of a centrifugal compressor for pressure ratio 4.5 ASME-2001-GT-314
紙規格・テクニカルリポート類
Feld, H.-J, Aschenbrenner, S, Girsberger, R2001<M-ASME-2001-GT-314>
国立国会図書館

Experimental investigation on the hydrogen peroxide fumigation into the inlet duct of a diesel engine SAE-2000-01-1919

Experimental investigation on the hydrogen peroxide fumigation into the inlet duct of a diesel engine SAE-2000-01-1919
紙規格・テクニカルリポート類
Gjirja, Savo, Olsson, Erik, Olsson, Lars-Ola, Ekman, Severin2000<M-SAE-2000-01-1919>
国立国会図書館

Benchmark experimental database for multiphase combustion model input and validation [microform] : characterization of the inlet combustion air / John F. Widmann, S. Rao Charagundla, Gary Presser (NISTIR ; 6370)

Benchmark experimental database for multiphase combustion model input and validation [microform] : characterization of the inlet combustion air / John F. Widmann, S. Rao Charagundla, Gary Presser (NISTIR ; 6370)
マイクロ図書
1999<YCA-C 13.58:6370>
国立国会図書館
  • 並列タイトル等（連結）Characterization of the inlet combustion air
  • 並列タイトル等Characterization of the inlet combustion air

Effect of the decaying overshoot of the Rankine vortex on the axial flow field behind the inlet guide vane of centrifugal compressors ASME-2000-GT-427

Effect of the decaying overshoot of the Rankine vortex on the axial flow field behind the inlet guide vane of centrifugal compressors ASME-2000-GT-427
紙規格・テクニカルリポート類
Chen, Y. N, Hagelstein, D, Kassens, I, Haupt, U, Rautenberg, M2000<M-ASME-2000-GT-427>
国立国会図書館

Flow measurements behind the inlet guide vane of a centrifugal compressor ASME-98-GT-86

Flow measurements behind the inlet guide vane of a centrifugal compressor ASME-98-GT-86
紙規格・テクニカルリポート類
Kassens, I, Rautenberg, M1998<M-ASME-98-GT-86>
国立国会図書館

Characterization of the inlet combustion air in NIST's reference spray combustion facility [microform] : effect of vane angle and Reynolds number / John F. Widmann, S. Rao Charagundla, Gary Presser (NISTIR ; 6458)

Characterization of the inlet combustion air in NIST's reference spray combustion facility [microform] : effect of vane angle and Reynolds number / John F. Widmann, S. Rao Charagundla, Gary Presser (NISTIR ; 6458)
マイクロ図書
2000<YCA-C 13.58:6458>
国立国会図書館

Overshoot of the Rankine vortex formed in the flow field behind the inlet guide vane of centrifugal compressors ASME-99-GT-182

Overshoot of the Rankine vortex formed in the flow field behind the inlet guide vane of centrifugal compressors ASME-99-GT-182
紙規格・テクニカルリポート類
Chen, Y. N, Hagelstein, D, Kassens, I, Hasemann, H, Haupt, U, Rautenberg, M1999<M-ASME-99-GT-182>
国立国会図書館

Analysis of the transonic flow at the inlet of a high pressure ratio centrifugal impeller ASME-98-GT-24

Analysis of the transonic flow at the inlet of a high pressure ratio centrifugal impeller ASME-98-GT-24
紙規格・テクニカルリポート類
Eisenlohr, Gernot, Dalbert, Peter, Krain, Hartmut, Proll, Hartwig, Richter, Franz-Arno, Rohne, Karl-Heinz1998<M-ASME-98-GT-24>
国立国会図書館

The effects of gasoline volatility on mass and composition of the inlet port wall film in port injected SI engines SAE-982517

The effects of gasoline volatility on mass and composition of the inlet port wall film in port injected SI engines SAE-982517
紙規格・テクニカルリポート類
Skippon, Stephen M, Norton, Daniel1998<M-SAE-982517>
国立国会図書館

The effect of the inlet boundary layer on the tip flow field in a transonic fan rotor ASME-98-GT-130

The effect of the inlet boundary layer on the tip flow field in a transonic fan rotor ASME-98-GT-130
紙規格・テクニカルリポート類
Takado, Junji, Sonoda, Toyotaka, Nakamura, Satoshi1998<M-ASME-98-GT-130>
国立国会図書館

Prediction of exhaust gas temperature at the inlet of an underbody catalytic converter during FTP-75 test SAE-972913

Prediction of exhaust gas temperature at the inlet of an underbody catalytic converter during FTP-75 test SAE-972913
紙規格・テクニカルリポート類
Cho, Yong-Seok, Kim, Chang-Rae, Kim, Duk-Sang, Lee, Jongwha, Lee, Soo-Won, Myung, Kwang-Hee, Choo, Jin-Seok1997<M-SAE-972913>
国立国会図書館

Two-dimensional LDV measurements in the inlet and exit manifolds of a single stage oxidizer turbine AIAA-97-0883

Two-dimensional LDV measurements in the inlet and exit manifolds of a single stage oxidizer turbine AIAA-97-0883
紙規格・テクニカルリポート類
Smith, A. W, Ramachandran, N1997<M-AIAA-97-0883>
国立国会図書館

Measurement of fuel droplet dynamics in the inlet port of an S.I. engine under firing conditions SAE-961924

Measurement of fuel droplet dynamics in the inlet port of an S.I. engine under firing conditions SAE-961924
紙規格・テクニカルリポート類
Almkvist, Goran, Dahlberg, Martin1996<M-SAE-961924>
国立国会図書館

Influence of the inlet port and combustion chamber configuration on the lean-burn behaviour of a spark-ignition gasoline engine SAE-960608

Influence of the inlet port and combustion chamber configuration on the lean-burn behaviour of a spark-ignition gasoline engine SAE-960608
紙規格・テクニカルリポート類
Kuhn, M, Abthoff, J, Kemmler, R, Kaiser, T1996<M-SAE-960608>
国立国会図書館

A study of Reynolds stresses and loss generation at the inlet to a centrifugal vaneless diffuser ASME-95-GT-150

A study of Reynolds stresses and loss generation at the inlet to a centrifugal vaneless diffuser ASME-95-GT-150
紙規格・テクニカルリポート類
Pinarbasi, Ali, Johnson, Mark W1995<M-ASME-95-GT-150>
国立国会図書館

Measurements of fuel film thickness in the inlet port of an S.I. engine by Laser Induced Fluorescence SAE-952483

Measurements of fuel film thickness in the inlet port of an S.I. engine by Laser Induced Fluorescence SAE-952483
紙規格・テクニカルリポート類
Almkvist, Goran, Denbratt, Ingemar, Josefsson, Goran, Mognusson, Ingemar1995<M-SAE-952483>
国立国会図書館

Effects of the inlet endwall boundary layer on 3-D flows and loss evolution in a linear turbine cascade ASME-95-GT-188

Effects of the inlet endwall boundary layer on 3-D flows and loss evolution in a linear turbine cascade ASME-95-GT-188
紙規格・テクニカルリポート類
Tominaga, J, Outa, E, Yamamoto, Atsumasa1995<M-ASME-95-GT-188>
国立国会図書館

Method for Extracting Forward Acoustic Wave Components from Rotating Microphone Measurements in the Inlets of Turbofan Engines. Final Contractor Report NASA-CR-195457 N95-30779 E-9577

Method for Extracting Forward Acoustic Wave Components from Rotating Microphone Measurements in the Inlets of Turbofan Engines. Final Contractor Report NASA-CR-195457 N95-30779 E-9577
マイクロ規格・テクニカルリポート類
1995<LS-N95/30779>
国立国会図書館
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