The discharge coefficients of the flow nozzles based on ASME PTC 6 are measured in a wide range of Reynolds number from Red = 5.8 × 104 to Red = 1.4 × 107, and the equations of the discharge coefficients are developed for the laminar, the transitional, and the turbulent flow ranges. The equation of the discharge coefficient consists of a nominal discharge coefficient and the tap effect. The nominal discharge coefficient is the discharge coefficient without tap, which is experimentally determined from the discharge coefficients measured for different tap diameters. The tap effects are correctly obtained by subtracting the nominal discharge coefficient from the discharge coefficient measured. The deviation of the present experimental results from the equations developed is from −0.06% to 0.04% for 3.0 × 106 < Red < 1.4 × 107 and from −0.11% to 0.16% for overall Reynolds number range examined. The developed equations are expected to be capable of estimating the discharge coefficient of the throat tap nozzle defined in PTC 6 with a high accuracy and contribute for the high accurate evaluation of steam turbines in power plants.
Skip Nav Destination
Article navigation
April 2016
Research-Article
Further Experiments and Investigations for Discharge Coefficient of PTC 6 Flow Nozzle in a Wide Range of Reynolds Number
Noriyuki Furuichi,
Noriyuki Furuichi
National Institute of Advanced
Industrial Science and Technology,
National Metrology Institute of Japan,
Tsukuba-Central 3, 1-1-1 Umezono,
Tsukuba 305-3563, Japan
e-mail: furuichi.noriyuki@aist.go.jp
Industrial Science and Technology,
National Metrology Institute of Japan,
Tsukuba-Central 3, 1-1-1 Umezono,
Tsukuba 305-3563, Japan
e-mail: furuichi.noriyuki@aist.go.jp
Search for other works by this author on:
Yoshiya Terao,
Yoshiya Terao
National Institute of Advanced
Industrial Science and Technology,
National Metrology Institute of Japan,
Tsukuba-Central 3, 1-1-1 Umezono,
Tsukuba 305-3563, Japan
e-mail: terao.yoshiya@aist.go.jp
Industrial Science and Technology,
National Metrology Institute of Japan,
Tsukuba-Central 3, 1-1-1 Umezono,
Tsukuba 305-3563, Japan
e-mail: terao.yoshiya@aist.go.jp
Search for other works by this author on:
Shinichi Nakao,
Shinichi Nakao
Flow Measurement Consulting
Laboratory Flow Col,
Youkoudai 4-27-7, Isogo-ku,
Yokohama 235-0045, Japan
e-mail: flowcol@flowcol.com
Laboratory Flow Col,
Youkoudai 4-27-7, Isogo-ku,
Yokohama 235-0045, Japan
e-mail: flowcol@flowcol.com
Search for other works by this author on:
Keiji Fujita,
Keiji Fujita
Flow Engineering Co., Ltd.,
Tsuruyacho 2-13-2,
Kanagawa-ku,
Yokohama 221-0835, Japan
e-mail: k-fujita@floweng.co.jp
Tsuruyacho 2-13-2,
Kanagawa-ku,
Yokohama 221-0835, Japan
e-mail: k-fujita@floweng.co.jp
Search for other works by this author on:
Kazuo Shibuya
Kazuo Shibuya
Flow Engineering Co., Ltd.,
Tsuruyacho 2-13-2,
Kanagawa-ku,
Yokohama 221-0835, Japan
e-mail: k-shibuya@floweng.co.jp
Tsuruyacho 2-13-2,
Kanagawa-ku,
Yokohama 221-0835, Japan
e-mail: k-shibuya@floweng.co.jp
Search for other works by this author on:
Noriyuki Furuichi
National Institute of Advanced
Industrial Science and Technology,
National Metrology Institute of Japan,
Tsukuba-Central 3, 1-1-1 Umezono,
Tsukuba 305-3563, Japan
e-mail: furuichi.noriyuki@aist.go.jp
Industrial Science and Technology,
National Metrology Institute of Japan,
Tsukuba-Central 3, 1-1-1 Umezono,
Tsukuba 305-3563, Japan
e-mail: furuichi.noriyuki@aist.go.jp
Yoshiya Terao
National Institute of Advanced
Industrial Science and Technology,
National Metrology Institute of Japan,
Tsukuba-Central 3, 1-1-1 Umezono,
Tsukuba 305-3563, Japan
e-mail: terao.yoshiya@aist.go.jp
Industrial Science and Technology,
National Metrology Institute of Japan,
Tsukuba-Central 3, 1-1-1 Umezono,
Tsukuba 305-3563, Japan
e-mail: terao.yoshiya@aist.go.jp
Shinichi Nakao
Flow Measurement Consulting
Laboratory Flow Col,
Youkoudai 4-27-7, Isogo-ku,
Yokohama 235-0045, Japan
e-mail: flowcol@flowcol.com
Laboratory Flow Col,
Youkoudai 4-27-7, Isogo-ku,
Yokohama 235-0045, Japan
e-mail: flowcol@flowcol.com
Keiji Fujita
Flow Engineering Co., Ltd.,
Tsuruyacho 2-13-2,
Kanagawa-ku,
Yokohama 221-0835, Japan
e-mail: k-fujita@floweng.co.jp
Tsuruyacho 2-13-2,
Kanagawa-ku,
Yokohama 221-0835, Japan
e-mail: k-fujita@floweng.co.jp
Kazuo Shibuya
Flow Engineering Co., Ltd.,
Tsuruyacho 2-13-2,
Kanagawa-ku,
Yokohama 221-0835, Japan
e-mail: k-shibuya@floweng.co.jp
Tsuruyacho 2-13-2,
Kanagawa-ku,
Yokohama 221-0835, Japan
e-mail: k-shibuya@floweng.co.jp
Contributed by the Controls, Diagnostics and Instrumentation Committee of ASME for publication in the JOURNAL OF ENGINEERING FOR GAS TURBINES AND POWER. Manuscript received July 28, 2015; final manuscript received July 31, 2015; published online October 21, 2015. Editor: David Wisler.
J. Eng. Gas Turbines Power. Apr 2016, 138(4): 041605 (11 pages)
Published Online: October 21, 2015
Article history
Received:
July 28, 2015
Revised:
July 31, 2015
Citation
Furuichi, N., Terao, Y., Nakao, S., Fujita, K., and Shibuya, K. (October 21, 2015). "Further Experiments and Investigations for Discharge Coefficient of PTC 6 Flow Nozzle in a Wide Range of Reynolds Number." ASME. J. Eng. Gas Turbines Power. April 2016; 138(4): 041605. https://doi.org/10.1115/1.4031310
Download citation file:
Get Email Alerts
Cited By
On Leakage Flows In A Liquid Hydrogen Multi-Stage Pump for Aircraft Engine Applications
J. Eng. Gas Turbines Power
A Computational Study of Temperature Driven Low Engine Order Forced Response In High Pressure Turbines
J. Eng. Gas Turbines Power
The Role of the Working Fluid and Non-Ideal Thermodynamic Effects on Performance of Gas Lubricated Bearings
J. Eng. Gas Turbines Power
Tool wear prediction in broaching based on tool geometry
J. Eng. Gas Turbines Power
Related Articles
Fluid Dynamics of a Pre-Swirl Rotor-Stator System
J. Turbomach (October,2003)
New Discharge Coefficient of Throat Tap Nozzle Based on ASME Performance Test Code 6 for Reynolds Number From 2.4 × 10 5 to 1.4 × 10 7
J. Fluids Eng (January,2014)
Influence of Reynolds Number on the Evolution of a Plane Air Jet Issuing From a Slit
J. Fluids Eng (October,2007)
The Discharge Coefficient of a Planar Submerged Slit-Jet
J. Fluids Eng (July,2003)
Related Proceedings Papers
Related Chapters
Antilock-Braking System Using Fuzzy Logic
International Conference on Mechanical and Electrical Technology, 3rd, (ICMET-China 2011), Volumes 1–3
Numerical Simulation of Internal Flow for Nozzle on Gasoline Direct Injection Engine
International Conference on Mechanical and Electrical Technology, 3rd, (ICMET-China 2011), Volumes 1–3
Cavitating Structures at Inception in Turbulent Shear Flow
Proceedings of the 10th International Symposium on Cavitation (CAV2018)