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Chee Tung

Experimental and Analytical Studies of a Model Helicopter Rotor in Hover
1980 · F. X. Caradonna, Chee Tung · NASA Technical Reports Server (NASA) · 387
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The Prediction of Transonic Flows on an Advancing Rotor
1986 · Chee Tung, Francis X. Caradonna, et al. · Journal of the American Helicopter Society · 90
Motion and Decay of a Vortex Ring
1967 · C. Tung, L. Ting · The Physics of Fluids · 86
Motion and Decay of a Vortex in a Nonuniform Stream
1965 · L. Ting, C. Tung · The Physics of Fluids · 76
Dynamic stall control for advanced rotorcraft application
1995 · Yung H. Yu, Soogab Lee, et al. · AIAA Journal · 72
The HART-II Test: Rotor Wakes and Aeroacoustics with Higher-Harmonic Pitch Control (HHC) Inputs - The Joint German/French/Dutch/US Project -
2002 · Heinz-Jürgen Pausder, Berend van der Wall, et al. · Vertical Flight Society Forum · 69
An experimental investigation of the parallel blade-vortex interaction
1984 · F. X. Caradonna, G. H. Laub, et al. · NASA STI Repository (National Aeronautics and Space Administration) · 68
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Compressible Dynamic Stall Control Using a Variable Droop Leading Edge Airfoil
2004 · M. S. Chandrasekhara, P. B. Martin, et al. · Journal of Aircraft · 62
The structure of trailing vortices generated by model rotor blades
1981 · Chee Tung, Sabina Pucci, et al. · NASA Technical Reports Server (NASA) · 59
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Aerodynamics and acoustics of rotor blade-vortex interactions
1995 · Yung H. Yu, Chee Tung, et al. · Journal of Aircraft · 54
Finite Difference Modeling of Rotor Flows Including Wake Effects
1984 · F. X. Caradonna, C. Tung, et al. · Journal of the American Helicopter Society · 44
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A Review of Rotor Wake Physics and Modeling
2011 · Narayanan M. Komerath, Marilyn J. Smith, et al. · Journal of the American Helicopter Society · 43
Dynamic Stall Alleviation Using a Deformable Leading Edge Concept-A Numerical Study
2003 · Mehmet Sahin, Lakshmi N. Sankar, et al. · Journal of Aircraft · 37
Numerical solution of the full-potential equation for rotors and oblique wings using a new wake model
1985 · I.-C. CHANG, C. TUNG · 23rd Aerospace Sciences Meeting · 32
Compressible Dynamic Stall Performance of a Variable Droop Leading Edge Airfoil with a Gurney Flap
2008 · M. S. Chandrasekhara, P. B. Martin, et al. · Journal of the American Helicopter Society · 31
Background oriented stereoscopic schlieren (BOSS) for full-scale helicopter vortex characterization
2000 · Markus Raffel, Chee Tung, et al. · elib (German Aerospace Center) · 31
The Prediction of Transonic Flows on Advancing Rotors
1984 · C. Tung, F.X. Caradonna, et al. · Vertical Flight Society Forum · 31
Performance and Flowfield Measurements on a 10-inch Ducted Rotor VTOL UAV
2004 · Preston Martin, Chee Tung · Vertical Flight Society Forum · 30
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Rotor hover performance prediction using a free-wake, computational fluid dynamics method
1989 · K. Ramachandran, C. Tung, et al. · Journal of Aircraft · 29
The prediction of transonic loading advancing helicopter rotors
1986 · Roger C. Strawn, Chee Tung · NASA STI Repository (National Aeronautics and Space Administration) · 26
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Suppression of dynamic stall with a leading-edge slat on a VR-7 airfoil
1993 · K. W. McAlister, Chee Tung · NASA Technical Reports Server (NASA) · 25
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The HART II Test in the LLF of the DNW - a Major Step towards Rotor Wake Understanding
2002 · Berend G. van der Wall, Bernd Junker, et al. · elib (German Aerospace Center) · 23
Geometric Analysis of Wing Sections
1995 · Chang, I-Chung, Torres, Francisco J., et al. · 22
HHC aeroacoustic rotor tests in the German-Dutch wind tunnel: Improving physical understanding and prediction codes
1998 · R. Kube, W.R. Splettstoesser, et al. · Aerospace Science and Technology · 21
Prediction and Measurement of Blade-Vortex Interaction Loading,
1995 · Chee Tung, Judith Gallman, et al. · 21
Works count: 104
Citation count: 1,877
H-index: 22
I10-index: 44
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