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C. P. "Case" van Dam Warren and Leta Giedt
Professor and Department Chair Department of Mechanical and Aerospace
Engineering Phone: (530) 752-7741 (direct) (530) 752-0580 (department) Fax: (530) 752-4158 Email: cpvandam@ucdavis.edu
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Professional Experience
July 2010 - Present
Warren and Leta Giedt Professor, Chair of the Department of Mechanical and Aerospace Engineering
March 2002 - Present
Director, California Wind Energy Collaborative (California Wind Energy Collaborative)
July 1985 - Present
Assistant Professor (1985 - 1989), Associate Professor (1989 - 1995) and Professor (1995 - Present) in the Department of Mechanical and Aeronautical Engineering of the University of California, Davis. Teaching undergraduate and graduate courses in a wide variety of subject areas including fluid-aerodynamics, aircraft design, and wind energy. Consultant for NASA, several aircraft companies, sailing yacht designers, and wind energy companies.
April - July 1992, June - December 1993, January - March 1996
Visiting Researcher at NASA Langley Research Center conducting research on high-lift aerodynamics in support of Subsonic Aircraft High-Lift Flight Project.
January 1984 - August 1985
Research Associate, Vigyan Research Associates, Inc., Hampton, Virginia. Worked on the design and optimization of advanced technology lifting systems with special emphasis on cruise drag and high-angle of-attack (stall/spin) lift characteristics. Also studied the shaping of airplane fuselages for minimum drag.
January - December 1983
NRC Postdoctorate at NASA Langley Research Center. Investigated the possibilities for and the potential benefits of extensive amounts of natural laminar flow on devices such as wingtip-mounted winglets.
Technical Interests
Research interests include:
· Aerodynamics including design and optimization
· Aircraft design
· Experimental and computational fluid dynamics
· Biofluiddynamics
· Wind energy
· Aero-hydrodynamics of sailing
Current research includes:
· Prediction, measurement and reduction of aerodynamic drag
· Multi-disciplinary design of aircraft high-lift systems
· In-flight infrared imaging of boundary-layer transition and separation
· Aerodynamics of wind turbines and aircraft at dynamic conditions
·
Micro-electro-mechanical systems for
aerodynamic load control
Also see links to Aero Research Group and California Wind Energy Collaborative.
Professional Activities and Honors
·
Honor Roll of Department of Aerospace
Engineering, University of Kansas, April 2010.
· Elected AIAA Associate Fellow, September 2007.
· U.S. Department of Energy award for "Outstanding Research and Development Partnership to Advance Wind Energy Technology" in partnership with Knight & Carver, and Sandia National Laboratories, May 2006.
· Associated Editor of Wind Energy for the international journal Solar Energy, Aug 2003 - July 2004.
· Member of Peer Review Panel to evaluate NASA research on Basic Aerodynamics, Langley Research Center, Hampton, VA, January 2004.
· Co-Director of Von Karman Institute for Fluid Dynamics Lecture Series on CFD-Based Aircraft Drag Prediction And Reduction, Rhode Saint Genese, Belgium, February 3-7, 2003.
· AIAA Fluids 2000 Art of Flow Control Artistic Award for Active Load Control and Lift Enhancement using MEM Translational Tabs, June 2000.
· Member of Peer Review Panel to evaluate NASA research on High-Lift Aerodynamics, Langley Research Center, Hampton, VA, November 1999.
· NASA Certificate of Recognition for work on In-Flight Infrared Surface Flow Visualization, October 1998.
· Member of Science Panel to review test of NREL research wind turbine in the NASA Ames 80' x 120' wind tunnel, Boulder, CO, October 1998.
· NASA-ASEE Summer Faculty Fellowship Awards, 1993 and 1994.
· Co-edited book titled Fluid Dynamics in Biology, Contemporary Mathematics, Vol. 141, 1993.
· Co-organized/co-chaired the AMS/IMS/SIAM Joint Summer Research Conference on Biofluiddynamics, University of Washington, Seattle, WA, July 6-12, 1991.
· NASA Certificate of Recognition for the development of Crescent Wing Planforms, December 1989.
· AIAA Lawrence Sperry Award for major innovative contributions in Applied Aerodynamics, 1989.
· NASA Certificate of Recognition for the development of an Aircraft Stall-Spin Entry Deterrent System, March 1988.
· Outstanding Advisor Award of the University of California, Davis, School of Engineering, 1985 - 1986.
· Group Achievement Award, Aerial Applications Research Team, NASA Langley Research Center, October 1983.
· National Research Council Postdoctoral Research Associateship Award, 1983.
· Member of Sigma Gamma Tau (National Honor Society in Aerospace Engineering).
Teaching
Undergraduate courses
· Aeronautical Engineering Fundamentals
· Applied Aircraft Aerodynamics
· Aircraft Performance
· Aircraft Preliminary Design
· Fluid Dynamics
· Mechanical Engineering Design Project
· Thermal Fluids Laboratory
Graduate courses
· Advanced Aerodynamics - Viscous Flow
· Advanced Aerodynamic Design and Optimization
· Aerodynamics of Flight Vehicles
· Advanced Wind-Tunnel Testing
· Wind Power Engineering
Short Courses
· Applied Aerodynamic Drag Reduction
· Aerodynamic Drag Reduction - Fundamentals and Applications
· High-Lift Systems & Aerodynamics for General Aviation and Subsonic Transport Aircraft
· Aerodynamic Design Improvements: High-Lift and Cruise
· Wind Energy for Technicians
· Wind Energy: A Technology and Industry Primer
·
Small Wind Energy Systems
Also see link to Aerospace Short Courses and CWEC Courses .
Patents
AIRCRAFT STALL-SPIN ENTRY DETERRENT SYSTEM, U.S. Patent No. 4,776,542, C.P. van Dam,
Issued October 11, 1988.
ACTIVE SYSTEM FOR CONTROL OF AERODYNAMIC
LOADING USING MICROFABRICATED TRANSLATIONAL TABS, U.S. Patent No. 7,028,954, C.P. van Dam, D.T. Yen, R.L. Smith, S.D. Collins,
Issued April 18, 2006.
METHOD AND APPARATUS FOR AUTOMATICALLY
GENERATING AIRFOIL PERFORMANCE TABLES, U.S.
Patent No. 7,124,038, C.P. van Dam, E.A. Mayda,
R.C. Strawn, Issued October 17, 2006.
WIND TURBINE WITH DEPLOYABLE AIR DEFLECTORS,
U.S. Patent No. 8,192,161, J.P. Baker, K.L. Jackson, E.A. Mayda, C.P. van Dam,
Issued June 5, 2012.
Selected Publications
FLIGHT EVALUATION OF THE EFFECT OF WINGLETS ON PERFORMANCE AND HANDLING QUALITIES OF SINGLE-ENGINE GENERAL AVIATION AIRPLANE, B. J. Holmes, C. P. van Dam, P. W. Brown, and P. L. Deal, NASA TM 81892, Dec. 1980.
LONGITUDINAL AERODYNAMIC CHARACTERISTICS OF
THE ATLIT AIRPLANE, J. Roskam, C. P. van Dam, and M. Griswold, Journal of
Aircraft, Vol. 18, No. 6, Jun. 1981, 495-496.
EFFECT OF WINGLETS ON PERFORMANCE AND
HANDLING QUALITIES OF GENERAL AVIATION AIRCRAFT, C. P. van Dam, B. J. Holmes
and C. Pitts, Journal of Aircraft, Vol. 18, No. 7, Jul. 1981, pp. 587-591.
AN EXPERIMENTAL AND THEORETICAL
INVESTIGATION OF DEPOSITION PATTERNS FROM AN AGRICULTURAL AIRPLANE, D. J.
Morris, C. C. Croom, C. P. van Dam, and B. J. Holmes, NASA TP 2348, Sep. 1984.
NATURAL LAMINAR FLOW AND AIRPLANE STABILITY
AND CONTROL, C. P. van Dam, Laminar Flow Aircraft Certification, NASA CP 2413,
Proceedings of a workshop held in Wichita, KS, Apr. 14-15, 1985.
SWEPT WING-TIP SHAPES FOR LOW-SPEED
AIRPLANES, C. P. van Dam, SAE Paper 851770, Oct. 1985 (SAE Transactions, Vol.
94, 1986, pp. 355).
EFFICIENCY CHARACTERISTICS OF CRESCENT-MOON
SHAPED WINGS AND CAUDAL FINS,C. P. van Dam, Nature,Vol. 325, No. 6103, Feb.
1987, pp. 435-437.
SHAPING OF AIRPLANE FUSELAGES FOR MINIMUM
DRAG, S. S. Dodbele, C. P. van Dam, P.M.H.W. Vijgen, and B. J. Holmes, Journal
of Aircraft, Vol. 24, No. 5, May 1987, pp. 298-304.
BOUNDARY-LAYER TRANSITION EFFECTS ON
AIRPLANE STABILITY AND CONTROL, C. P. van Dam, and B. J. Holmes, Journal of
Aircraft, Vol. 25, No. 8, Aug. 1988, pp. 702-709.
EFFECTS OF COMPRESSIBILITY ON DESIGN OF
SUBSONIC NATURAL LAMINAR FLOW FUSELAGES, P.M.H.W. Vijgen, S. S. Dodbele, B. J.
Holmes, and C. P. van Dam, Journal of Aircraft, Vol. 25, No. 9, Sep. 1988, pp.
776-784.
IN WIND AND WATER, C. P. van Dam, The
Sciences, Jan-Feb. 1988, pp. 36-39.
KEEL DESIGN FOR LOW VISCOUS DRAG, C. J.
Obara, and C. P. van Dam, Journal of Ship Research, Vol. 33, No. 2, Jun. 1989,
pp. 145-155.
SHEARED WING-TIP AERODYNAMICS: WIND-TUNNEL
AND COMPUTATIONAL INVESTIGATION, P.M.H.W. Vijgen, C. P. van Dam, and B. J.
Holmes, Journal of Aircraft, Vol. 26, No. 3, Mar. 1989, pp. 207-213.
WIND-TUNNEL INVESTIGATIONS OF WINGS WITH
SERRATED SHARP TRAILING EDGES, P.M.H.W. Vijgen, C. P. van Dam, B. J. Holmes,
and F. G. Howard, Low Reynolds Number Aerodynamics, Lecture Notes in Engineering,
No. 54, T. J. Mueller (Ed.), Springer-Verlag, 1989, pp. 295-313.
KEELS AND RUDDERS WITH HIGHLY SWEPT TIPS, C.
P. van Dam, P.M.H.W. Vijgen, and C. J. Obara, SailTech-89, Vol. 35, Western Periodicals
Company, Proceedings of the 18th Annual Conference on Sailing Technology held
at Stanford University, CA, Oct. 14-15, 1989.
COMPARISON OF ITERATIVE AND DIRECT SOLUTION
METHODS FOR VISCOUS FLOW PROBLEMS, C. P. van Dam, and M. Hafez, AIAA Journal,
Vol. 27, No. 10, Oct. 1989, pp. 1459-1461.
UNSTEADY VISCOUS FLOW CALCULATIONS INCLUDING
SURFACE HEATING AND COOLING EFFECTS, C. P. van Dam, M. Hafez, D. Brucker, and
S. Elli, Notes on Numerical Fluid Mechanics, P. Wesseling (Ed.), Vol. 29,
Vieweg, 1990, pp.79-88.
CALCULATIONS OF VISCOUS FLOW WITH SEPARATION
USING NEWTON'S METHOD AND DIRECT SOLVER, C. P. van Dam, M. Hafez, J. Ahmad,
AIAA Journal, Vol. 28, No. 5, May 1990, pp. 938-940.
CALCULATION AND MEASUREMENT OF INDUCED DRAG
AT LOW SPEEDS, C. P. van Dam, K. Nikfetrat, P.M.H.W. Vijgen, and C. M. Fremaux,
SAE Paper 901935, Oct. 1990.
COMMENT ON "OPTICAL BOUNDARY-LAYER
TRANSITION DETECTION IN A TRANSONIC WINDTUNNEL," P.M.H.W. Vijgen, C. P.
van Dam, and C. J. Obara, AIAA Journal, Vol. 28, No. 12, Dec. 1990, pp.
2142-2143.
AERODYNAMIC CHARACTERISTICS OF CRESCENT AND
ELLIPTIC WINGS AT HIGH ANGLES OF ATTACK, C. P. van Dam P.M.H.W. Vijgen, and B.
J. Holmes, Journal of Aircraft, Vol. 28, No. 4, Apr. 1991, pp. 253-260.
THE INFLUENCE OF A LAMINAR SEPARATION BUBBLE
ON BOUNDARY-LAYER STABILITY, S. Elli, and C. P. van Dam, AIAA Paper 91-3294,
Sep. 1991.
EXPERIMENTAL INVESTIGATION ON THE EFFECT OF
CRESCENT PLANFORM ON LIFT AND DRAG, C. P. van Dam, P.M.H.W. Vijgen, and B. J.
Holmes, Journal of Aircraft, Vol. 28, No. 11, Nov. 1991, pp. 713-720.
THE INFLUENCE OF BULGES ON BOUNDARY-LAYER
INSTABILITY, S. Elli, C. P. van Dam, and K. Nikfetrat, 5th Symposium on
Numerical and Physical Aspects of Aerodynamic Flows, Long Beach, CA, Jan.
13-16, 1992.
SUBSONIC AND TRANSONIC LOW-REYNOLDS-NUMBER
AIRFOILS WITH REDUCED PITCHING MOMENTS, J. Reuther, C. P. van Dam, and R.
Hicks, Journal of Aircraft, Vol. 29, No. 3, May-Jun. 1992, pp. 297-298.
ACCURATE PREDICTION OF DRAG USING EULER
METHODS, C. P. van Dam, and K. Nikfetrat, Journal of Aircraft, Vol. 29, No. 3,
May-Jun. 1992, pp. 516-519.
SIMULATION OF NONLINEAR TOLLMIEN-SCHLICHTING
WAVE GROWTH THROUGH A LAMINAR SEPARATION BUBBLE, C. P. van Dam, and S. Elli,
Instability, Transition, and Turbulence, M. Y. Hussaini, A. Kumar and C. L.
Streett (Eds.), Springer-Verlag, 1992, pp. 311-321.
TURBULENCE EFFECTS ON THE DESIGN AND
PERFORMANCE OF LOW-DRAG KEELS, P.M.H.W. Vijgen, C. P. van Dam, and C. J. Obara,
Journal of Ship Research, Vol. 36, No. 3, Sep. 1992, pp. 268-279.
LIFT AND DRAG CALCULATIONS FOR WINGS AND
TAILS: TECHNIQUES AND APPLICATIONS, C. P. van Dam, K. Nikfetrat, and P.M.H.W.
Vijgen, Contemporary Mathematics, Vol. 141, 1993, pp. 463-477.
COMPARISON OF PREDICTIONS OF AIRFOIL
CHARACTERISTICS FOR THE NREL S805 AND S809 AIRFOILS, D. B. Bernadett, and C. P.
van Dam, Proceedings of the Windpower '93 Conference, San Francisco, CA, Jul.
1993, pp. 290-298.
ACCURATE DRAG PREDICTION - A PREREQUISITE
FOR DRAG REDUCTION RESEARCH, K.J. Wong, T.K. Ayers, and C.P. van Dam, SAE Paper
932571, Sep. 1993 (SAE Transactions, Section 1, Vol. 102, 1993, pp. 1882-1891).
IN-FLIGHT PRESSURE DISTRIBUTIONS AND
SKIN-FRICTION MEASUREMENTS ON A SUBSONIC TRANSPORT HIGH-LIFT WING SECTION, L.P.
Yip, J.D. Hardin, P.M.H.W. Vijgen, and C.P. van Dam, High-Lift System
Aerodynamics, AGARD CP-515, Sep.1993, pp. 21-1 thru 21-19.
APPLIED AERODYNAMICS, C.P. van Dam,
Aerospace America, Dec. 1993, pp. 12-13.
AIRFOIL SHAPING FOR REDUCED RADAR CROSS
SECTION, H. Vinh, C.P. van Dam, and H.A. Dwyer, Journal of Aircraft, Vol. 31,
No. 4, Jul-Aug. 1994, pp. 787-793.
NUMERICAL STUDY ON THE EFFECT OF TIP-CAP
SHAPE ON WING AERODYNAMIC CHARACTERISTICS, K.J. Wong and C.P. van Dam, AIAA
Paper 95-0042, Jan. 1995.
THE NASA B737-100 HIGH-LIFT PROGRAM -
MEASUREMENTS AND COMPUTATIONS, L.P. Yip, C.P. van Dam, J.H. Whitehead, J.D.
Hardin, S.J. Miley, R.C. Potter, A. Bertelrud, D.D. Edge, and P.E. Willard,
Aeronautical Journal, Vol. 99, No. 989, Nov. 1995, pp. 372-386.
IN-FLIGHT PRESSURE MEASUREMENTS ON A
SUBSONIC TRANSPORT HIGH-LIFT WING SECTION, L.P. Yip, P.M.H.W. Vijgen, J.D.
Hardin, and C.P. van Dam, Journal of Aircraft, Vol. 32, No. 3, May- Jun. 1995,
pp. 529-538.
DRAG PREDICTION AT SUBSONIC AND TRANSONIC
SPEEDS USING EULER METHODS, C.P. van Dam, K. Nikfetrat, K. Wong, and P.M.H.W.
Vijgen, Journal of Aircraft, Vol. 32, No. 4, Jul-Aug. 1995, pp. 839-845.
SLAT TRANSITION CHARACTERISTICS ON THE NASA
B737-100 AIRCRAFT USING INFRARED IMAGING AND HOT-FILM ANEMOMETRY, S.J. Miley,
C.P. van Dam, L.P. Yip, P.E. Willard, J.P. Crowder, and R.L. Watzlavick, Flow
Visualization VII, J. Crowder (Ed.), Begell House, Sep. 1995, pp. 950-956.
FINITE DIFFERENCE MAXWELL SOLVER TO STUDY
GEOMETRIC SHAPE EFFECTS ON RADAR SIGNATURE, H. Vinh, C.P. van Dam, and H.A.
Dwyer, Journal of Aircraft, Vol. 34, No. 1, Jan-Feb. 1997, pp. 56-63.
IN-FLIGHT BOUNDARY-LAYER MEASUREMENTS ON A
HIGH-LIFT SYSTEM: SLAT, C.P. van Dam, S.M. Los, S.J. Miley, V.E. Roback, L.P.
Yip, A. Bertelrud, and P.M.H.W. Vijgen, Journal of Aircraft, Vol. 34, No. 6,
Nov-Dec. 1997, pp. 748-756.
IN-FLIGHT BOUNDARY-LAYER MEASUREMENTS ON A
HIGH-LIFT SYSTEM: MAIN ELEMENT AND FLAP, C.P. van Dam, S.M. Los, S.J. Miley,
V.E. Roback, L.P. Yip, A. Bertelrud, and P.M.H.W. Vijgen, Journal of Aircraft,
Vol. 34, No. 6, Nov-Dec. 1997, pp. 757-763.
STATISTICAL ANALYSIS OF IN-FLIGHT HOT-FILM
SIGNALS OF TRANSITIONAL FLOWS, S.M. Los, and C.P. van Dam, AIAA Paper 98-2440,
Jun. 1998.
REMOTE IN-FLIGHT INFRARED IMAGING FOR
ANALYZING SURFACE FLOWS, D.W. Banks, C.P. van Dam, and H.J. Shiu, NASA Tech
Briefs, Sep. 1998, p. 76.
GURNEY FLAP EXPERIMENTS ON AIRFOIL AND
WINGS, C.P. van Dam, D.T. Yen, and P.M.H.W. Vijgen, Journal of Aircraft, Vol.
36, No.2, Mar-Apr. 1999, pp. 484-486.
AIRFOIL DRAG PREDICTION AND DECOMPOSITION,
D.D. Chao, and C.P. van Dam, Journal of Aircraft, Vol. 36, No. 4, Jul-Aug.
1999, pp. 675-681.
AERO-MECHANICAL DESIGN METHODOLOGY FOR
SUBSONIC CIVIL TRANSPORT HIGH-LIFT SYSTEMS, C.P. van Dam, S.G. Shaw, J.C.
Vander Kam, R.R. Brodeur, P.K.C. Rudolph, and D. Kinney, NATO Research &
Technology Agency Applied Vehicle Technology Panel Symposium on Aerodynamic
Design and Optimization of Flight Vehicles in a Concurrent Multi-Disciplinary
Environment, Ottawa, Canada, Oct. 18-21, 1999.
AERO-MECHANICAL DESIGN OF HIGH-LIFT SYSTEMS,
C.P. van Dam, S.G. Shaw, J.C. Vander Kam, P.K.C. Rudolph, and D. Kinney,
Aircraft Engineering and Aerospace Technology, Vol. 71, No. 5, 1999, pp.
436-443.
RECENT EXPERIENCE WITH DIFFERENT METHODS OF
DRAG PREDICTION, C.P. van Dam, Progress in Aerospace Sciences, Vol. 35, No. 8,
Nov. 1999, pp. 751-798.
ACTIVE LOAD CONTROL AND LIFT ENHANCEMENT
USING MEM TRANSLATIONAL TABS, D.T. Yen, C.P. van Dam, F. Bräeuchle, R.L. Smith,
and S.D. Collins, AIAA Fluids 2000, AIAA Paper 2000-2422, Denver, CO, Jun.
2000.
VISUALIZATION OF IN-FLIGHT FLOW PHENOMENA
USING INFRARED THERMOGRAPHY, D.W. Banks, C.P. van Dam, H.J. Shiu, and G.M.
Miller, NASA TM-2000-209027, Jul. 2000.
COMPUTATIONAL STUDY OF ROTARY TESTS ON
FOREBODY MODELS, C.P. van Dam,. T. Dal Bello, E. Duque, C.M. Fremaux, AIAA
Atmospheric Flight Mechanics Conference, AIAA paper 2000-4105, Denver, CO, Aug.
14-17, 2000.
WIND TURBINES, C.P. van Dam, McGraw-Hill
Yearbook of Science & Technology 2002, McGraw-Hill, New York, 2001, pp.
413-416.
ACTIVE LOAD CONTROL FOR AIRFOILS USING
MICROTABS, D.T. Yen Nakafuji, C.P. van Dam, R.L.Smith, and S.D. Collins,
Journal of Solar Energy Engineering, Vol. 123, No. 4, Nov. 2001, pp. 282-289.
TRANSITION PREDICTION FOR A TWO-DIMENSIONAL
NAVIER-STOKES SOLVER APPLIED TO WIND-TURBINE AIRFOILS, R.R. Brodeur, and C.P.
van Dam, Wind Energy, Vol. 4, No. 2, 2001, pp. 61-75.
DESIGN-ORIENTED HIGH-LIFT METHODOLOGY FOR
GENERAL AVIATION AND CIVIL TRANSPORT AIRCRAFT, C.P. van Dam, J.C. Vander Kam,
and J.K. Paris, Journal of Aircraft, Vol. 38, No. 6, Nov-Dec. 2001, pp. 1076-1084.
BUBBLE INDUCED UNSTEADINESS ON A WIND
TURBINE AIRFOIL, E.A. Mayda, C.P. van Dam, Journal of Solar Energy Engineering,
Vol. 124, NO. 4, Nov. 2002, pp. 335-344
THE AERODYNAMIC DESIGN OF MULTI-ELEMENT HIGH-
LIFT SYSTEMS FOR TRANSPORT AIRPLANES, C.P. van Dam, Progress in Aerospace
Sciences, Vol. 38, No.2, 2002, pp. 101-144.
IN-FLIGHT VISUALIZATION OF SUPERSONIC FLOW
TRANSITION USING INFRARED IMAGING, C.P. van Dam, H.J. Shiu, D.W. Banks,
R.R.Tracy, and J. Chase, Journal of Aircraft, Vol. 39, No. 6, Nov-Dec. 2002,
pp. 936-944.
BLADE-WAKE INTERACTION NOISE FOR TURBINES
WITH DOWNWIND ROTORS, G.M. McNerney, C.P. van Dam, D.T. Yen-Nakafuji, Journal
of Solar Energy Engineering, Vol. 125, No. 4, Nov. 2003, pp. 497-505.
AERODYNAMIC ANALYSIS OF BLUNT TRAILING EDGE
AIRFOILS, K.J. Standish and C.P. van Dam, Journal of Solar Energy Engineering,
Vol. 125, No. 4, Nov. 2003, pp. 479-487.
SIMULATION OF FLOW ABOUT ROTATING FOREBODIES
AT HIGH ANGLES OF ATTACK, S. Saephan, C.P. van Dam, C.M. Fremaux, and T.
DalBello, Journal of Aircraft, Vol. 41, No. 6, Nov-Dec. 2004, pp. 1298-1305.
INNOVATIVE DESIGN APPROACHES FOR LARGE WIND
TURBINE BLADES, K. Jackson, M. Zuteck, C.P. van Dam, K.J. Standish, and D. Berry,
Wind Energy, Vol. 8, No. 2, Apr-Jun. 2005, pp. 141-171.
COMPUTATIONAL ANALYSIS OF A MICRO-TAB BASED
AERODYNAMIC LOAD CONTROL SYSTEM FOR ROTOR BLADES, K.J. Standish and C.P. van
Dam, Journal of the American Helicopter Society, Vol. 50, No. 3, Jul. 2005, pp.
249- 258.
AUTOMATIC GENERATION OF AIRFOIL PERFORMANCE
TABLES USING A TWO-DIMENSIONAL NAVIER-STOKES SOLVER, E.A. Mayda and C.P. van
Dam, Journal of the American Helicopter Society, Vol. 50, No. 4, Oct. 2005, pp.
338-348.
WING DRAG PREDICTION AND DECOMPOSITION, D.D.
Chao and C.P. van Dam, Journal of Aircraft, Vol. 43, No. 1, Jan-Feb. 2006, pp.
82-90.
UNSTEADY COMPUTATIONAL INVESTIGATIONS OF
DEPLOYING LOAD CONTROL TABS, R. Chow and C.P. van Dam, Journal of Aircraft,
Vol. 43, No. 5, Sep-Oct. 2006, pp. 1458-1469.
EXPERIMENTAL ANALYSIS OF A THICK BLUNT
TRAILING EDGE WIND TURBINE AIRFOIL, J.P. Baker, E.A. Mayda, and C.P. van Dam,
Journal of Solar Energy Engineering, Vol. 128, No. 4, Nov. 2006, pp. 422-431.
DESIGN AND NUMERICAL OPTIMIZATION OF THICK
AIRFOILS, T. Winnemoller and C.P. van Dam, Journal of Aircraft, Vol. 44, No. 1,
Jan-Feb. 2007, pp. 232-240.
TWO-DIMENSIONAL WIND TUNNEL AND
COMPUTATIONAL INVESTIGATION OF A MICROTAB MODIFIED AIRFOIL, J.P. Baker, K.J
Standish, and C.P. van Dam, Journal of Aircraft, Vol. 44, No. 2, Mar-Apr. 2007,
pp. 563-572.
COMPUTATIONAL AERODYNAMIC ANALYSIS OF AN
INBOARD BLUNT TRAILING EDGE MODIFICATION TO THE NREL PHASE VI ROTOR, D.D. Chao
and C.P. van Dam, Wind Energy, Vol. 10, No. 6, Nov-Dec. 2007, pp. 529-550.
DETERMINATION OF WING-ONLY AIRCRAFT TUMBLING
CHARACTERISTICS THROUGH COMPUTATIONAL FLUID DYNAMICS, S. Saephan and C.P. van
Dam, Journal of Aircraft, Vol. 45, No. 3, May-Jun. 2008, pp. 1044-1053.
ON THE TEMPORAL RESPONSE OF ACTIVE LOAD
CONTROL DEVICES, R. Chow, C.P. van Dam, Wind Energy, Vol. 13, No. 2-3, 2010,
pp. 135-149.
AN OVERVIEW OF ACTIVE LOAD CONTROL
TECHNIQUES FOR WIND TURBINES WITH AN EMPHASIS ON MICROTABS, S.J. Johnson, J.P.
Baker, C.P. van Dam, D.E. Berg, Wind Energy, Vol. 13, No. 2-3, 2010, pp.
239-253.
BALANCING FATIGUE DAMAGE AND TURBINE
PERFORMANCE THROUGH INNOVATIVE PITCH CONTROL ALGORITHM, S. Johnson, S. Larwood,
G. McNerney, C.P. van Dam, Wind Energy, Vol. 15, No. 5, 2012, pp. 665-825.
VERIFICATION OF COMPUTATIONAL SIMULATIONS OF
THE NREL 5-MW ROTOR WITH A FOCUS ON INBOARD FLOW SEPARATION, R. Chow, C.P. van
Dam, accepted for publication in Wind Energy, 2012.
COMPUTATIONAL INVESTIGATIONS OF BLUNT
TRAILING EDGE AND TWIST MODIFCATIONS TO THE INBOARD REGION OF THE NREL 5-MW
ROTOR, R. Chow, C.P. van Dam, accepted for publication in Wind Energy, 2012.
DYNAMIC ANALYSIS TOOL DEVELOPMENT FOR SWEPT
WIND TURBINE BLADES, S. Larwood, C.P. van Dam, accepted for publication in Wind
Energy, 2012.
Last modified: September 8, 2012