Tianshu Liu
ADDRESS:
Department
of Mechanical and Aeronautical Engineering
G-220 Parkview Campus
Western Michigan University
Kalamazoo, MI 49008-5343
Phone: (269) 276-3426, Fax: (269) 276-3421
E-mail: tianshu.liu@wmich.edu
RESEARCH INTERESTS:
Aerodynamics, Fluid Mechanics, Heat
Transfer, Measurement Techniques and Instrumentation Applied to Aerospace
Engineering and Sciences
CURRENT POSITION:
9/2004-Now Associate
Professor, Director of
Applied Aerodynamics Laboratory
Department of Mechanical and Aeronautical
Engineering
G-220 Parkview Campus
Western Michigan University
Kalamazoo, MI 49008-5343
Specific Research Areas:
Experimental
and applied aerodynamics, theoretical aerodynamics models, advanced image-based
aerodynamic measurement techniques for various quantities (surface pressure,
temperature/heat transfer, skin friction, velocity fields, and integrated
forces), videogrammetric techniques and vision for aerospace applications,
flapping flight, flight vehicle design, transition and turbulence, flow
controls, flight tests
WORK EXPERIENCE:
9/99-9/2004 Research
Scientist
Aerodynamics,
Aerothermodynamics and Acoustics Competency (AAAC)
NASA Langley Research
Center (LaRC), Hampton, VA 23681, USA
Performed Studies:
(1)
Flapping Wing and Unsteady Wake Topology; (2) Design Methodologies for Flapping
MAVs; (3) Nano-Optic Sensor for Skin Friction; (4) Separation and Wake Control
of Airfoils Using Responsive Skin; (5) Mechanism and Prevention of Frost Formation
on Model Surface in National Transonic Facility (NTF); (6) Videogrammetric
Measurements of Shape and Dynamics of Solar Sails and Large Space Structures;
(7) Columbia Debris Transport; (8) Intelligent Expert System for Aerodynamic
Design.
Principal Investigator, Flapping flight and agile MAVs,
FY 2002, NASA MSB Branch Fund
Principal Investigator, Building universal foundations
for image-based measurements of motion fields and morphology of deformable
matters, FY 2001, NASA Creativity & Innovation Program (C&I)
Principal Investigator, Computer vision as a universal
framework for image-based measurements in aerospace engineering and sciences,
FY 2001, NASA Intelligent Synthesis Environment (ISE) Program
Principal Investigator, Optical
measurements of static and dynamics aerodynamic loads, FY 2001, NASA
Integrated Instrumentation and Technologies System (IITS) Program
Principal Investigator, Optical
measurements of static and dynamics aerodynamic loads, FY 2000, NASA
Integrated Instrumentation and Technologies System (IITS) Program
Principal Investigator, Artificial intelligent vision, FY2000,
NASA Intelligent Synthesis Environment (ISE) Program
2/97-9/99 Research
Scientist, High Technology Corporation, Hampton, VA 23666, USA
Principal Investigator, Advanced photogrammetric systems for measurements of position and dynamic aeroelastic deformation of wind-tunnel models (1998 NASA SBIR Phase I)
Principal Investigator, Further improvements of a single camera
photogrammetric system and data-processing software for model deformation
measurements (1999 NASA contract)
Principal Investigator, Lifetime-based pressure-sensitive paint imaging system and its integration with model deformation measurement system (1999 NASA SBIR Phase I)
Key Investigator, Involved the NASA ADTE program for
unification of modern aerodynamic measurement techniques in a single
wind-tunnel test
1/96-2/97 Postdoctoral
Research Assistant, Purdue University, Indiana, USA
Luminescent oil-film skin friction meter.
Pressure and temperature measurements on
rotating blades in turbine engine using luminescent paints.
Boundary-layer transition detection
methods on aerodynamic models in cryogenic wind tunnels using
temperature-sensitive luminescent paints.
Development of cryogenic pressure- and
temperature-sensitive paint system.
2/96 Visiting Scientist, Japanese National Aerospace Laboratory (NAL),
Tokyo, Japan
Boundary-layer transition detection on
airfoils in the NAL cryogenic wind tunnel using luminescent paints.
8/91-12/95 Research
Assistant, Purdue University, Indiana, USA
Development of a system of temperature-
and pressure-sensitive luminescent paints for aerodynamic testing.
Study of flow and heat transfer
structures in an acoustically-excited circular impinging jet.
Study of heat transfer distributions on a
waverider model in hypersonic flows using temperature-sensitive paints.
Study of shock/turbulent-boundary-layer
interactions using temperature-sensitive paints.
Study of temperature and heat transfer
distributions on a hot-film sensor in a flat-plate turbulent boundary layer.
Random vortex-tube model for small-scale
turbulence and the asymptotic probability density distribution of the
dissipation rate.
Exact solution of the Navier-Stokes
equation ¾ Non-orthogonal stagnation flow on the
surface of a quiescent fluid.
Design
of the test section of the Purdue/Boeing subsonic wind tunnel.
11/88-8/90 Researcher,
University of Houston, Houston, USA
Non-linear
fundamental-subharmonic wave interaction in an axisymmetric jet.
Instantaneous
vorticity measurements using a nine-hotwire probe.
12/85-11/88 Lecturer,
Nanjing University of Aeronautics and Astronautics, China
Boundary-layer transition control.
Study
of horseshoe vortices generated by heat pulses in a boundary layer.
Control of the leading-edge vortices of a
delta wing by introducing controllable perturbations.
5/85-12/85 Visiting
Scientist, DLR Institute of Fluid Mechanics at Göttingen, Germany
Study of three-dimensional instability of
a flat-plate laminar boundary layer by means of heat-pulsing arrays.
EDUCATION:
PhD
(1996), Aeronautics and Astronautics, Purdue University, USA
MS
(1985), BS (1982), Aerodynamics, Nanjing University of Aeronautics and
Astronautics, China
PROFESSIONAL SERVICES:
Reviewer for
AIAA Journal, AIAA Journal of Aircraft, AIAA Journal of Thermophysics and Heat
Transfer, Experiments in Fluids, Measurement Sciences and Technology, Physics
of Fluids, Review of Scientific Instruments, The Journal of The American
Acoustics Socity, NASA SBIR Phase I and II, NASA Institute for Advanced
Concepts Phase II
INVITED PRESENTATIONS:
“A
Unified View of Image-Based Measurements in Aerospace Applications”,
Keynote Speech at the International Workshop on Molecular Imaging for
Interdisciplinary Research, Tohoku University, Sendai, Japan, Nov. 8-9, 2004
“Comparative
Scaling of Flapping- and Fixed-Wing Flyers”, 2003 Bioflight Workshop, NASA
Langley Research Center (LaRC), Hampton, Virginia, August 7, 2003
“Pressure
and Temperature Sensitive Paints”, AIAA Short Course, St. Louis, Missouri, June,
2002
“Image-Based
Techniques for Wind Tunnel Testing”, George Washington University, Washington
DC, April 8, 2002
“Pressure
Sensitive Paints ¾
Theories and Practices”,
Keynote Speech at the Workshop on Molecular Sensors for Aero-Thermodynamic Research,
Nagoya University, Nagoya, Japan, March 13, 2001
“Luminescent
Molecule Sensors in Fluid Mechanics and Heat Transfer”, The University of
Western Ontario, London, Canada, October 16, 1997
“TSP
and PSP Developments at Purdue”, NASA Langley Research Center (LaRC),
Hampton, Virginia, December 21, 1996
“Temperature-
and Pressure-Sensitive Paints in Aerodynamics”, Japanese National Aerospace
Laboratory (NAL), Tokyo, February 20, 1996
PUBLICATIONS:
Book and Book Chapter:
T.
Liu and J. P. Sullivan, Pressure and Temperature Sensitive Paints
(Experimental Fluid Mechanics), Springer-Verlag, Berlin (2004)
T. Jones, A. A. Dorrington, J. R.
Blandino, C. Fraser and T. Liu, Photogrammetric Measurement Methods (Chapter
5), Gossamer Structures, AIAA Press, Washington
DC (2005) (in press)
Refereed
Archival Publication:
T. Liu, “Comparative
scaling of flapping- and fixed-wing flyers”, AIAA Journal (in review), (2005)
T. Liu, “Time-area-averaged
momentum stream tube theory for flapping flight”, AIAA Journal (in review) (2005)
T. Liu, K. Kuykendoll, R. Rhew and S. Jones, “Avian wing geometry and kinematics”, AIAA Journal (in review) (2005)
T. Liu, A. W. Burner and R. Pappa, “Photogrammetric techniques for aerospace
applications”, Progress in Aerospace
Sciences, (2005) (in preparation)
T. Liu, “Optimum
bifurcating-tube tree for gas transport”, Journal
of Fluids Engineering, Vol. 127, No. 3, pp. 550-553 (2005)
T. Liu, “Geometric
and kinematic aspects of image-based measurements of deformable bodies”, AIAA Journal, Vol. 42, No. 9, pp.
1910-1920, (2004)
T. Liu and J. Sullivan, “In-situ calibration
uncertainty of pressure-sensitive paint”, AIAA Journal, Vol. 41, No. 11, pp. 2300-2302, (2003)
T.
Liu, “Pressure-correction method for low-speed
pressure-sensitive paint measurements”, AIAA
Journal, Vol. 41, No. 5, pp. 906-911, (2003)
T.
Liu, D. Barrows, A.
Burner and R. Rhew, “Determining
aerodynamic loads based on optical deformation measurements”, AIAA Journal, Vol. 40, No. 6, pp.
1105-1112, (2002)
T.
Liu, T. Togerson, J.
Sullivan, R. Johnston, and S. Fleeter, “Transonic
rotor blade pressure measurement using fluorescent paint”, Journal of Propulsion and Power, Vol.
18, No. 2, pp. 491-493, (2002)
A. Burner, T. Liu, S. Garg, T. Ghee and N. Taylor, “Aeroelastic deformation measurements of flap, gap and overhang on a
semispan model”, Journal of Aircraft,
Vol. 38, No. 6, pp. 1147-1154, (2001)
T.
Liu, N. Teduka, M.
Kameda and K. Asai, “Diffusion timescale
of porous pressure-sensitive paint”, AIAA
Journal, Vol. 39, No. 12, pp. 2400-2402, (2001)
A. Burner and T. Liu, “Videogrammetric
model deformation measurement technique”, Journal of Aircraft, Vol. 38, No. 4, pp. 745-754, (2001)
T.
Liu and T. Finley, “Estimating bias error distribution”, Review of Scientific Instruments, Vol.
72, No. 9, pp. 3561-3571, (2001)
T.
Liu, M. Guille and J.
Sullivan, “Accuracy of pressure
sensitive paint”, AIAA Journal,
Vol. 39, No. 1, pp. 103-112, (2001)
T.
Liu, L. Cattafesta, R.
Radezsky and A. W. Burner, “Photogrammetry
applied to wind tunnel testing”, AIAA
Journal, Vol. 38, No. 6, pp. 964-971, (2000)
A.W. Burner, T. Liu, S. Garg, J.H. Bell, and D.G. Morgan, “Unified model deformation and flow transition measurements”, Journal of Aircraft, Vol. 36, No. 5, pp.
898-901, (1999)
L. Cattafesta, T. Liu and J. Sullivan, “Uncertainty
estimates for temperature sensitive paint measurements with CCD cameras”, AIAA
Journal, Vol. 36, No. 11, pp. 2102-2108 (1998)
T.
Liu and J. Sullivan, “Luminescent oil-film skin friction meter”,
AIAA Journal, Vol. 36, No. 8, pp.
1460-1465 (1998)
T.
Liu, B. Campbell, S.
Burns and J. Sullivan, “Temperature- and
pressure-sensitive paints in aerodynamics”, Applied Mechanics Reviews, Vol. 50, No. 4, pp. 227-246 (1997)
K. Asai, H. Kanda, T. Kunimasu, T. Liu and J. Sullivan, “Detection of boundary layer transition in a
cryogenic wind tunnel by using luminescent paint”, Journal of Aircraft, Vol. 34, No. 1, pp. 34-42 (1997)
T.
Liu and J. Sullivan, “Heat transfer and flow structures in an
excited circular impinging jet”, International
Journal of Heat and Mass Transfer, Vol. 39, No. 17, pp. 3695-3706 (1996)
T.
Liu, B. Campbell and J.
Sullivan, “Heat transfer measurement on
a waverider at Mach 10 using fluorescent paint”, Journal of Thermophysics and Heat Transfer, Vol. 9, No. 4, pp.
605-611 (1995)
T.
Liu, B. Campbell and J.
Sullivan, “Fluorescent paint for
measurement of heat transfer in shock/turbulent boundary layer interaction”,
Experimental Thermal and Fluid Science,
10, pp. 101-112, (1995)
T.
Liu, B. Campbell and J.
Sullivan, “Surface temperature of a hot
film on a wall in shear flow”, International
Journal of Heat and Mass Transfer, Vol. 37, No. 17, pp. 2809-2814 (1994)
T.
Liu, “A note on the probability distribution of
the dissipation rate in locally isotropic turbulence”, Physics of Fluids A 5(9), pp. 2234-2238 (1993)
T.
Liu, “Non-orthogonal stagnation flow on the
surface of a quiescent fluid ¾
An exact solution of the Navier-Stokes equation”, Quarterly
of Applied Mathematics, Vol. L, No. 1, pp. 39-47, March (1992)
T.
Liu, S. Shi and M. D.
Zhou, “Horseshoe vortices generated by
heat pulses in boundary layer”,
Journal of Experimental Mechanics, Vol. 4, No. 3, pp. 290-296 (1989)
C. Dai, T. Liu, Y. Teng and M. Xiao, “Measuring
techniques for wall shearing stress in turbulent boundary-layer”, ACTA AERONAUTICA ET ASTRONAUTICA SINICA,
Vol. 9, No. 5, pp. 203-210 (1988)
M. D. Zhou and T. Liu, “Stability
investigation in nominally two-dimensional laminar boundary layer by means of
heat pulsing”, Perspectives in
Turbulence Studies, Ed. H. U. Meier and P. Bradshaw, Springer-Verlag,
Berlin (1987)
Conference Papers:
T. Liu, “Videogrammetric determination of aircraft position and attitude
for vision-based autonomous landing”, 44th AIAA Aerospace Sciences Meeting and
Exhibit, Reno, January (2006) (submitted)
T.
Liu, “A unified view of image-based measurements
in aerospace applications”, Proceedings of MOSAIC, the International
Workshop on Molecular Imaging for Interdisciplinary Research, Tohoku
University, Sendai, Japan, (2004)
T.
Liu, K. Kuykendoll, R.
Rhwe and S. Jones, “Avian wings”, AIAA Paper 2004-2186, Portland, Oregon (2004)
T.
Liu, “Geometric, kinematic and radiometric
aspects of image-based measurements”, AIAA
Paper 2002-3239, St. Louis, MO, June, (2002)
A. W. Burner, T. Liu, and R. DeLoach, “Uncertainty
of videogrammetric techniques used for aerodynamic testing”, AIAA Paper 2002-2794, St. Louis, MO, June,
(2002)
P. A. Parker and T. Liu, “Uncertainty
analysis of the single-vector force balance calibration system”, AIAA Paper 2002-2792, St. Louis, June,
(2002)
T.
Liu and T. Finley, “Estimating bias error distribution”, AIAA Paper 2001-0162, Reno, Jan., (2001)
T.
Liu, D. Barrows, A.
Burner and R. Rhew, “Determining
aerodynamic loads based on optical deformation measurements”, AIAA Paper 2001-0560, Reno, Jan., (2001)
T. Amer, T. Liu and D. Oglesby, “Characterization
of pressure sensitive paint intrusiveness effects on aerodynamic data”, AIAA Paper 2001-0556, Reno, Jan., (2001)
A. W. Burner, T. Liu, S. Garg, T. A. Ghee and N. J. Taylor, “Aeroelastic deformation measurements of flap, gap and overhang on a
semispan model”, AIAA Paper
2000-2386, Denver, June, (2000)
T.
Liu, S. Garg, N.
Lachendro, M. Guille, and J. Sullivan, “Lifetime
methods for pressure sensitive paints”, Proceeding of the 7th PSP Workshop,
Purdue University, Oct. 11-13, 1999.
T.
Liu, R. Radeztsky, S.
Garg and L. Cattafesta, “A
videogrammetric model deformation system and its integration with pressure
paint”, AIAA Paper 99-0568, Reno,
January, (1999)
T.
Liu, R. Radeztsky, S.
Garg and L. Cattafesta, “A photogrammetric
model deformation system and its integration with pressure paint”, 1998 Pressure Sensitive Paint (PSP) Workshop,
Boeing Company, Seattle, WA, October, (1998)
T.
Liu and J. Sullivan, “Applications of Temperature and Pressure
Sensitive Paints”, AGARD Conference
Proceedings CP-601: Advanced Aerodynamic Measurement Technology, presented
at the 81st Meeting and Symposium of the Fluid Dynamics Panel, Seattle,
WA, 22-25 September, (1997)
S. Torgerson, T. Liu and J. Sullivan, “Rotor
blade pressure measurement in a rotating machinery using pressure and
temperature sensitive paints”, AGARD
Conference Proceedings CP-598: Advanced Non-Intrusive Instrumentation for
Propulsion Engines, presented at the
Propulsion and Energetics Panel (PEP)
90th Symposium, Brussels, Belgium, 20-24 October, (1997)
A.W. Burner, R. Radeztsky and T. Liu, “Videometric Applications in Wind Tunnels”, SPIE’s International Symposium on Optics, Imaging and Instrumentation,
San Diego, California, USA (1997)
T.
Liu and J. Sullivan, “Luminescent oil-film skin friction meter”,
AIAA Paper 97-2216 (1997)
T.
Liu, R. Johnston, S.
Torgerson, S. Fleeter and J. Sullivan, “Rotor
blade pressure measurement in a high speed axial compressor using pressure and
temperature sensitive paints”, AIAA
Paper 97-0162 (1997)
Torgerson, S. D., Liu, T. and Sullivan, J. P., “Use
of pressure sensitive paints in low speed flows”, AIAA Paper 96-2184, (1996)
K. Asai, H. Kanda, T. Kunimasu, T. Liu and J. Sullivan, “Detection of boundary layer transition in a
cryogenic wind tunnel by using luminescent paint”, AIAA Paper 96-2185, (1996)
T.
Liu, B. Campbell and J.
Sullivan, “Accuracy of temperature
sensitive fluorescent paint for heat transfer measurement”, AIAA paper 95-2042, (1995)
T.
Liu, B. Campbell and J.
Sullivan, “Remote surface temperature
and heat transfer mapping for a waverider model at Mach 10 using fluorescent
paint”, AIAA Paper 94-2484 (1994)
B. Campbell, T. Liu and J. Sullivan, “Temperature
sensitive fluorescent paint systems”, AIAA
Paper 94-2483 (1994)
M. Hamner, B. Campbell, T. Liu and J. Sullivan, “A scanning laser system for temperature and
pressure sensitive paint”, AIAA Paper
94-0728 (1994)
T.
Liu, B. Campbell and J.
Sullivan, “Thermal paints for
shock/boundary layer interaction in inlet flow”, AIAA Paper 92-3626 (1992)
B. Campbell, T. Liu and J. Sullivan, “Temperature
measurement using fluorescent molecules”, Sixth International Symposium on Applications of Laser Techniques to
Fluid Mechanics, Lisbon, Portugal (1992)
Technical
Reports:
T.
Liu, “Geometric, kinematic and radiometric aspects of image-based
measurements”, The
Finial Report for NASA C&I Program, (2001)
T.
Liu, “Computer vision as a universal framework for image-based measurements in
aerospace engineering and sciences”, The
Finial Report for NASA ISE Program, (2000)
T.
Liu and H. U. Meier, “Artificial boundary-layer transition
generated by heat pulses”, DFVLR
IB222-86 A21 (1986)
T.
Liu and H. U. Meier, “Measurements of drag coefficients for
screens and lattices”, DFVLR IB222-85
A33 (1985)