Cryogenic helium-4 has extremely small kinetic viscosity, which makes it a promising material for high Reynolds (Re) number turbulence research in compact laboratory apparatus. In its superfluid phase (He II), helium has an extraordinary heat transfer capability and has been utilized in various scientific and engineering applications. In order to unlock the full potential of helium in turbulence research and to improve our understanding of the heat transfer mechanism in He II, a flow facility that allows quantitative study of helium heat-and-mass transfer processes is needed. Here, we report our work in assembling and testing a unique helium pipe-flow facility that incorporates a novel double-line molecular tagging velocimetry (DL-MTV) system. This flow facility allows us to generate turbulent pipe flows with Re above 107, and it can also be adapted to produce heat-induced counterflow in He II. The DL-MTV system, which is based on the generation and tracking of two parallel thin molecular tracer lines with an adjustable separation distance, allows us to measure not only the velocity profile but also both the transverse and longitudinal spatial velocity structure functions. We have also installed a differential pressure sensor on the flow pipe for pressure drop measurements. The testing results of the flow facility and the measuring instruments are presented. We discuss how this facility will allow us to solve some outstanding problems in the helium heat-and-mass transfer topic area.
Skip Nav Destination
,
,
,
,
,
CHORUS
Article navigation
Research Article|
May 08 2020
A cryogenic-helium pipe flow facility with unique double-line molecular tagging velocimetry capability
Hamid Sanavandi
;
Hamid Sanavandi
1
Department of Mechanical Engineering, FAMU-FSU College of Engineering, Florida State University
, Tallahassee, Florida 32310, USA
2
National High Magnetic Field Laboratory, Florida State University
, 1800 E Paul Dirac Dr., Tallahassee, Florida 32310, USA
Search for other works by this author on:
Shiran Bao
;
Shiran Bao
1
Department of Mechanical Engineering, FAMU-FSU College of Engineering, Florida State University
, Tallahassee, Florida 32310, USA
2
National High Magnetic Field Laboratory, Florida State University
, 1800 E Paul Dirac Dr., Tallahassee, Florida 32310, USA
Search for other works by this author on:
Yang Zhang
;
Yang Zhang
1
Department of Mechanical Engineering, FAMU-FSU College of Engineering, Florida State University
, Tallahassee, Florida 32310, USA
3
Florida Center for Advanced Aero-Propulsion, Florida State University
, 2003 Levy Ave., Tallahassee, Florida 32310, USA
Search for other works by this author on:
Ruben Keijzer;
Ruben Keijzer
2
National High Magnetic Field Laboratory, Florida State University
, 1800 E Paul Dirac Dr., Tallahassee, Florida 32310, USA
Search for other works by this author on:
Wei Guo
;
Wei Guo
a)
1
Department of Mechanical Engineering, FAMU-FSU College of Engineering, Florida State University
, Tallahassee, Florida 32310, USA
2
National High Magnetic Field Laboratory, Florida State University
, 1800 E Paul Dirac Dr., Tallahassee, Florida 32310, USA
a)Author to whom correspondence should be addressed: [email protected]
Search for other works by this author on:
Louis N. Cattafesta, III
Louis N. Cattafesta, III
1
Department of Mechanical Engineering, FAMU-FSU College of Engineering, Florida State University
, Tallahassee, Florida 32310, USA
3
Florida Center for Advanced Aero-Propulsion, Florida State University
, 2003 Levy Ave., Tallahassee, Florida 32310, USA
Search for other works by this author on:
Hamid Sanavandi
1,2
Shiran Bao
1,2
Yang Zhang
1,3
Ruben Keijzer
2
Wei Guo
1,2,a)
Louis N. Cattafesta, III
1,3
1
Department of Mechanical Engineering, FAMU-FSU College of Engineering, Florida State University
, Tallahassee, Florida 32310, USA
2
National High Magnetic Field Laboratory, Florida State University
, 1800 E Paul Dirac Dr., Tallahassee, Florida 32310, USA
3
Florida Center for Advanced Aero-Propulsion, Florida State University
, 2003 Levy Ave., Tallahassee, Florida 32310, USA
a)Author to whom correspondence should be addressed: [email protected]
Rev. Sci. Instrum. 91, 053901 (2020)
Article history
Received:
March 18 2020
Accepted:
April 18 2020
Connected Content
Citation
Hamid Sanavandi, Shiran Bao, Yang Zhang, Ruben Keijzer, Wei Guo, Louis N. Cattafesta; A cryogenic-helium pipe flow facility with unique double-line molecular tagging velocimetry capability. Rev. Sci. Instrum. 1 May 2020; 91 (5): 053901. https://doi.org/10.1063/5.0008117
Download citation file:
Pay-Per-View Access
$40.00
Sign In
You could not be signed in. Please check your credentials and make sure you have an active account and try again.
Citing articles via
Long-range spin wave imaging with nitrogen vacancy centers and time resolved magneto-optical measurements
Carolina Lüthi, Lukas Colombo, et al.
Overview of the early campaign diagnostics for the SPARC tokamak (invited)
M. L. Reinke, I. Abramovic, et al.
An instrumentation guide to measuring thermal conductivity using frequency domain thermoreflectance (FDTR)
Dylan J. Kirsch, Joshua Martin, et al.
Related Content
Liquid helium inertial jet for comparative study of classical and quantum turbulence
Rev. Sci. Instrum. (November 2011)
Visualization of He II forced flow around a cylinder
Physics of Fluids (April 2015)
Producing and imaging a thin line of He 2 ∗ molecular tracers in helium-4
Rev. Sci. Instrum. (September 2015)
Particle dynamics in wall-bounded thermal counterflow of superfluid helium
Physics of Fluids (June 2017)