This paper analyses a novel heat transfer enhancement technique that can be used in compressors to limit the temperature rise during compression. This technique is based on the injection of external high-pressure gas into the chamber during the compression process. The impact of different factors on the effectiveness of this technique has been studied using experimental and computational methods. In the first set of trials, the location and angle of injection of the external air was varied. It was observed that the heat transfer coefficient governing the heat transfer rate from the chamber varied greatly with change in location and angle of injection. In the second set of experiments, the source pressure of the injected gas was varied from 100.66 kPa to 551.58 kPa. It was observed that the temperature rise of air in the chamber was reduced with an increase in source pressure. Additionally, the increase in chamber pressure was steeper in the higher source pressure cases. In the third set of experiments, the injection profile of the injected gas was varied. This parameter did not greatly impact the effectiveness of external gas injection. In the last set of experiments, the time of initiation of injection was varied. Earlier injection had a positive impact on reducing the temperature rise in the chamber. However, the pressure in the chamber was seen to increase more rapidly in the runs with early injection. Considering that these factors could have a positive/negative impact on the temperature and pressure in the chamber (work required for compression), it may be required to optimize the injection of external high-pressure gas depending on the application.
Skip Nav Destination
Article navigation
June 2017
Technical Briefs
Analysis of a Novel Technique for Temperature Rise Abatement in Liquid Piston Compressors–External Gas Injection
Hari Subramaniam Bhaskaran,
Hari Subramaniam Bhaskaran
Department of Mechanical and Aerospace Engineering,
North Carolina State University,
Raleigh, NC 27606
e-mail: hsubram2@ncsu.edu
North Carolina State University,
Raleigh, NC 27606
e-mail: hsubram2@ncsu.edu
Search for other works by this author on:
Paul Ro,
Paul Ro
Department of Mechanical and Aerospace Engineering,
North Carolina State University,
Raleigh, NC 27606
e-mail: ro@ncsu.edu
North Carolina State University,
Raleigh, NC 27606
e-mail: ro@ncsu.edu
Search for other works by this author on:
Joong-Kyoo Park,
Joong-Kyoo Park
Department of Mechanical and Aerospace Engineering,
North Carolina State University,
Raleigh, NC 27606
e-mail: jpark15@ncsu.edu
North Carolina State University,
Raleigh, NC 27606
e-mail: jpark15@ncsu.edu
Search for other works by this author on:
Kishore Ranganath Ramakrishnan
Kishore Ranganath Ramakrishnan
Department of Mechanical and Aerospace Engineering,
North Carolina State University,
Raleigh, NC 27606
e-mail: kramakr4@ncsu.edu
North Carolina State University,
Raleigh, NC 27606
e-mail: kramakr4@ncsu.edu
Search for other works by this author on:
Hari Subramaniam Bhaskaran
Department of Mechanical and Aerospace Engineering,
North Carolina State University,
Raleigh, NC 27606
e-mail: hsubram2@ncsu.edu
North Carolina State University,
Raleigh, NC 27606
e-mail: hsubram2@ncsu.edu
Paul Ro
Department of Mechanical and Aerospace Engineering,
North Carolina State University,
Raleigh, NC 27606
e-mail: ro@ncsu.edu
North Carolina State University,
Raleigh, NC 27606
e-mail: ro@ncsu.edu
Joong-Kyoo Park
Department of Mechanical and Aerospace Engineering,
North Carolina State University,
Raleigh, NC 27606
e-mail: jpark15@ncsu.edu
North Carolina State University,
Raleigh, NC 27606
e-mail: jpark15@ncsu.edu
Kishore Ranganath Ramakrishnan
Department of Mechanical and Aerospace Engineering,
North Carolina State University,
Raleigh, NC 27606
e-mail: kramakr4@ncsu.edu
North Carolina State University,
Raleigh, NC 27606
e-mail: kramakr4@ncsu.edu
1Corresponding author.
Contributed by the Heat Transfer Division of ASME for publication in the JOURNAL OF THERMAL SCIENCE AND ENGINEERING APPLICATIONS. Manuscript received February 4, 2016; final manuscript received December 20, 2016; published online March 15, 2017. Assoc. Editor: Samuel Sami.
J. Thermal Sci. Eng. Appl. Jun 2017, 9(2): 024503 (13 pages)
Published Online: March 15, 2017
Article history
Received:
February 4, 2016
Revised:
December 20, 2016
Citation
Bhaskaran, H. S., Ro, P., Park, J., and Ramakrishnan, K. R. (March 15, 2017). "Analysis of a Novel Technique for Temperature Rise Abatement in Liquid Piston Compressors–External Gas Injection." ASME. J. Thermal Sci. Eng. Appl. June 2017; 9(2): 024503. https://doi.org/10.1115/1.4035969
Download citation file:
Get Email Alerts
Cited By
Experimental and Finite Element Investigations to Study the Temperature Distribution at the Orthotic Boot–Skin Interface
J. Thermal Sci. Eng. Appl (July 2025)
Proposal and Evaluation of a Novel Solar Thermal-Driven Cooling-Power Cogeneration System
J. Thermal Sci. Eng. Appl (July 2025)
Aero-Thermal Calculations for a Rotor Blade With Different Dimple and Protrusion Arrangements
J. Thermal Sci. Eng. Appl (July 2025)
Related Articles
Performance Improvements in Cooker-Top Gas Burners for Small Aspect Ratio Changes
J. Thermal Sci. Eng. Appl (December,2017)
Nanofluid-based counterflow immersion cooling for lithium-ion battery during fast charging
J. Thermal Sci. Eng. Appl (January,0001)
Computational Fluid Dynamics and Experimental Analysis of the Heat Transfer in a Room With a Roof Solar Chimney
J. Thermal Sci. Eng. Appl (April,2022)
Numerical Analysis of Thermal Performance in a 5 by 5 Battery Pack Configured with PCM and Optimized Fin Layout
J. Thermal Sci. Eng. Appl (January,0001)
Related Proceedings Papers
Related Chapters
Later Single-Cylinder Engines
Air Engines: The History, Science, and Reality of the Perfect Engine
Pulsation and Vibration Analysis of Compression and Pumping Systems
Pipeline Pumping and Compression Systems: A Practical Approach, Second Edition
Pulsation and Vibration Analysis of Compression and Pumping Systems
Pipeline Pumping and Compression System: A Practical Approach, Third Edition