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MAE Faculty and Staff Directory
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to Hsun-Hu Chen
Research & Publications
Dr.
Hsun-Hu Chen
Recent
Publications
- H.H. Chen and T. Cebeci, “Predictions of Ice Shapes
on Wings and Multi-Element Airfoils,” AIAA Paper
94-0608, 1994.
- T. Cebeci, H. H. Chen and D. Arnal, “Natural Transition
in Compressible Flows on Wings: Spatial Theory and Experiment,”
AIAA Paper 94-0824, 1994.
- T. Cebeci, H. H. Chen and K. Kaups,” Linear Stability
Analysis of Three-dimensional Flows with Surface Curvature:
Effects of Sweep Angle and Reynolds Number,” AIAA
Paper 94-0827, 1994.
- J. Shin, B. Berkowitz, H. H. Chen and T. Cebeci, “Prediction
of Ice Shapes and Their Effect on Airfoil Drag” Journal
of Aircraft, Vol. 31, No. 2, pp. 263-270, 1994.
- T. Cebeci, H. H. Chen and B. P. Lee, "Calculation
of Three-dimensional Low Reynolds Number Flows," Journal
of Aircraft, Vol. 31, No. 3, pp. 564-571, 1994.
- H. H. Chen, M.F. Platzer and T. Cebeci, “Analysis
of Airfoils at Low Reynolds Numbers,” presented at the
Seventh International Symposium on Unsteady Aerodynamics and
Aeroelasticity of Turbomachines, Fukuoka, Japan, Sep. 25-29,
1994.
- H. H. Chen and T. Cebeci, “The Role of Turbulence
Models in Predicting the Stall and Post-stall Behavior of
Airfoils,” presented at the Sixth Asian Congress of
Fluid Mechanics, Singapore, May 22-26, 1995.
- T. Cebeci, H. H. Chen and E. Besnard, “The Role of
Zarf in Predicting Transition in Three-dimensional Flows with
the Saddle-Point Method,” presented at Colloquium of
the Royal Netherlands Academy of Arts and Sciences: Transition
Boundary Layers in Aeronautics, Amsterdam, Dec. 6-8, 1995.
- T. Cebeci, E. Besnard and H. H. Chen, “Calculation
of Multi-Element Airfoil Flows, Including Flap Wells”
AIAA Paper 96-0056.
- A. Verhoff, H. H. Chen and T. Cebeci, “An Accurate
and Efficient Interactive Boundary Layer Method to Analysis
and Design of Airfoils,” AIAA paper 96-0328.
- G. T. Tzong, H. H. Chen, K. C. Chang and T. Cebeci, “A
General Interface Method for Aeroelastic Analysis of Aircraft,”
presented at the NASA Computational Aerosciences Workshop,
Aug. 13-15, 1996.
- G. T. Tzong, H. H. Chen, K. C. Chang, T. Wu, and T. Cebeci,
“A General Method for Calculating Aero-Structures Interaction
on Aircraft Configurations,” AIAA Paper No. 96-3892,
1996.
- T. Cebeci and H. H. Chen, “An interactive Boundary-Layer
Method for Aerodynamic Flows,” Chapter 6 in Flows
at Large Reynolds Numbers, Computational Mechanics Publications,
1997.
- H. H. Chen, K. C. Chang, G. T. Tzong and T. Cebeci, “Aeroelastic
Analysis of Wing and Wing/Fuselage Configurations,”
AIAA Paper No. 98-0907, 1998.
- E. Besnard, A. Schmitz, G. Tzong, K. Kaups, H. Hefazi,
J. Hess, H. H. Chen and T. Cebeci, “Hydrofoil Design
and Optimization for Fast Ships,” Report AE-98-1,
Aerospace Engineering Department, California State University,
Long Beach, CA, Jan. 1998.
- G. Tzong, H. Chen and T. Cebeci, ”An Integrated Structural
Optimization Tool for Aircraft,” presented at the Australasian
Conference on Structural Optimisation, Feb. 11-13, 1998.
- T. Cebeci, E. Besnard and H. H. Chen, “An Interactive
Boundary Layer Method for Multi-Element Airfoils,” Computers
& Fluids, Vol. 27, No. 5-6, PP. 651-661, 1998.
- E. Besnard, A. Schmitz, K. Kaups, G. Tzong, H. Hefazi,
H. H. Chen, O. Kural and T. Cebeci, “Hydrofoil Design
and Optimization for Fast Ships,” 1998 ASME International
Congress and Exhibition, Anaheim, CA, Nov. 1998.
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