Dr. Robert T. Nagel short RESUME
Personal: Address: 6309 Valley Estates Dr.
Raleigh, N. C. 27612
Birthplace: Pittsburgh, Pennsylvania
Academic position: Professor, Associate department Head & Director of Graduate Program
: Mechanical and Aerospace Engineering
Box 7910
North Carolina State University
Raleigh, N. C. 227695
919-***-**** abpqdx@r.postjobfree.com
Education:
Ph.D. University of Connecticut. 1980. Mechanical Engineering
M.S. Pennsylvania State University. 1972. Aerospace Engineering
B.S. Pennsylvania State University. 1970. Aerospace Engineering
Employment Experience:
2004 present Professor, Associate Depart. Head and Director of the Graduate Program, North Carolina
State University, Mechanical & Aerospace Eng.
2001 2004 Professor, Mechanical & Aerospace Eng. and Director of the Aerospace Program, North
Carolina State University
1991 -2001 Professor, Director of the Center for Sound and Vibration, North Carolina State University,
Mechanical & Aerospace Eng. .
1983-1991 Associate Professor, North Carolina State University, Mechanical & Aerospace Eng.
1980-1983 Assistant Professor, North Carolina State University, Mechanical & Aerospace Eng.
1977-1980 Lecturer in Mechanical Engineering, University of Connecticut. Responsible for
coordinating and teaching an upper division course in measurement techniques.
1972-1977 Analytical Engineer in the Noise Reduction Group at Pratt & Whitney Aircraft Connecticut
Operations. Responsible for formulating analytical models of: fan, turbine and core engine
noise generation, propagation and radiation phenomena. and for developing prediction
systems for these types of noise.
Professional Consulting:
Consultant for 57 companies / organizations between 1993 and 2009.
Sample Research Experience:
Study and Validation of Propulsion Airframe Aeroacoustics effects from Aircraft Configurations: NIAG-00-
VAR-OTH, NASA, 8/15/02 12/31/05.
Preparing the 21st Century Workforce NIA based consortium, 2005.
NIA Base Funding Research Plan, $300K, 10-01-02, NIA/NASA Langley, 2002-03
National Institute for Aerospace program funding, NASA Langley, Base Budget for five years 9/02 to 9-07 at
$1.21Million per year for NC State.
Fan noise investigation from Caterpillar Corp, 2001- present..
2
Development of Environmental test Chamber, for Underwriters Lab April 2000 Dec. 2001.
Grease removal from an Exhaust Flow with Acoustic Means, Captive-Aire Systems Inc., Dec. 1998 - Dec. 1999.
ATS (STTR through NASA Lewis) Active Noise Control of General Aviation Propellers, Sept. 1995 - August
1996.
Culp Lumber Co. - New London, NC. Reversible Fan Evaluation, June 1993 - Dec. 1995
NASA Lewis, Aerodynamic and Acoustic Interaction of Counter - Rotating Propellers January 1988-July 1993.
Academy of Model Aeronautics, Model Propeller Noise Reduction, January 1988 - August 1989.
McDonnell Douglas Corp., "Aerodynamic Interaction Noise of Counter Rotation Propellers", December 1986-
June 1990.
NASA Langley, "Enhanced Viscous Flow Drag Reduction Using Acoustic ExcitationMarch 1986-March 1987.
NASA Langley, "The Effects of Amplitude and Phase of Acoustic Excitation of a LEBU Device on Viscous flow
Drag Reduction, February 1, 1985-February 1, 1986.
NASA Langley, "Viscous flow Drag Reduction by Acoustic Excitation of a LEBU", $, November 1983-
February 1985.
"Design and Construction of a Low Speed Boundary Layer Wind Tunnel", March 1983-1984.
NASA Lewis, "The Effects of Supersonic Jet Screech Tone Reduction on Broadband Shock-Associated Noise",
September 1981-February 1983.
Invited speaker research presentations
Near Field Propeller Noise Control International Conference on Nonlinear Problems in Aviation and
Aerospace, May 10-12, 2000, Daytona Beach, FL.
Sample Publications:
Journals;
Active Control of Far-Field Noise from a Ducted Propeller, with Dan Sutliff, AIAA Journal, Vol. 33, No. 2,
1995, pp. 231 - 236.
Development of an Active Noise Control system for Ducted fans (without Acoustic Feedback) with Dan
Sutliff, Proceedings of 2nd Conference on Recent Advances in Active Control of Sound & Vibration, pg. 825-
836, Technomic Publishing, April 28-30, 1993.
"Aerodynamic Interaction Tones of a Model Counter - Rotating Propeller", AIAA Journal, April 1988, Vol. 26,
No. 4, pp. 498-500.
"The NCSU Low Speed Boundary Layer Wind Tunnel, SAE Transactions, 1985, Vol. 6, pp. 6.760-6.768.
"Supersonic Jet Screech Tone Cancellation", AIAA Journal, Vol. 21, No. 11, November 1983, pp. 1541-1545.
"Reflection of Sound by a Boundary Layer", Journal of Sound and Vibration, Vol. 85, No. 1, 1982, pp. 31-38.
"Boundary Layer Effects on Sound in a Circular Duct", Journal of Sound and Vibration, Vol. 85, No. 1, 1982,
pp. 19-29.
"Review of Theory and Methods for Turbine Noise Prediction", Progress in Astronautics and Aeronautics,
1976, Vol. 46, pp. 155-176.
3
"Inlet Geometry and Axial Mach Number Effects on Fan Noise Propagation", Progress in Astronautics and
Aeronautics, 1975, Vol. 38, pp. 73-94.
Papers;
Near Field Propeller Noise Control, Proceedings of the International Conference on Nonlinear Problems in
Aviation & Aerospace, Vol. 2, Pg. 505-512, European Conference Publications, 2001.
Active Noise Control of an Unducted Model Propeller, AIAA Paper CEAS/AIAA-97-1639,
3rd AIAA/CEAS Aeroacoustics Conference; proceedings, pg. 441 - 447, May 12 - 14 1997, Atlanta, GA, with
B. J. Ikelheimer.
"Active Noise Control of Multiple Acoustic Modes in a Circular Duct," AIAA Paper 96-1781, 2nd
AIAA/CEAS Aeroacoustics Conference,(17th AIAA Aeroacoustics Conference). May 6-8, 1996, State
College, PA., with B. J. Ikelheimer.
"Synthesis of Spinning Modes for Active Noise Control," AIAA Paper CEAS/AIAA-95-033, 1st Joint
CEAS/AIAA Aeroacoustics Conference, (16th AIAA Aeroacoustics Conference) Munich, Germany, June 12-
15, 1995, with B. J. Ikelheimer.
"Active Control of Far-Field Noise from a Ducted Propeller" AIAA Paper 93-4356, AIAA Aeroacoustics
Conference. Long Beach, CA. Oct. 25, 1993, with Daniel L. Sutliff
"Forward Rotor Vortex Effects on Counter-Rotating Propeller Noise", AIAA Paper No. 92-02-153,
DGLR/AIAA Aeroacoustics Conference. Aachen Germany, May, 1992.
Flow Interaction & Noise from a Counter Rotating Propeller, AIAA Paper 91-0596, 29th AIAA Aerospace
Sciences meeting, Reno, NV. Jan. 7 - 10, 1991
Interaction between Rotors of a Counter Rotating Propeller, AIAA Paper 90-3976, 13th AIAA Aeroacoustics
Conference, Tallahassee, Fl. Oct., 22-24, 1990
Effects of Rotor Spacing on Aerodynamic Interaction and Noise of Counter-Rotating Propellers, 10th Brazilian
Congress of Mechanical Engineering, Rio de Janeiro, Dec. 1989.
Relating Flow and Noise in Counter Rotating Propellers, AIAA paper 89-1145, April, 1989.
"Boundary Layer Control by Acoustic Excitation", AIAA Paper No. 86-1954, July 1986.
"The NCSU Low Speed Boundary Layer Wind Tunnel, SAE Paper 851897, 1985.
"An Experimental Study of Supersonic Jet Shock-Associated Noise", AIAA Paper No. 83-0708, 1983.
"Effects of Leading Edge Serrations on Noise Radiation from a Model Rotor", AIAA Paper No. 72-655, 1972.
Magazines articles (6 total None shown)
Meetings, Conferences & Symposia ( 33 total none shown)
4
Professional Activities:
PATENTS AWARDED:
US Patent #6652274B2 Kiln-related structures and associated methods Issued 2003
US Patent # 6393723 Forced Convection Heat Exchanger for Kilns. Issued 2002
US Patent # 6370792 Structure & Method for Introducing Air into a Kiln . Issued 2002
US Patent # 5488785 Controlled Upper Row Airfoil. Issued 1996
US Patent # 5437109 Aerodynamic Surfacing. Issued 1995
US Patent # 5416985 Multi track Center Bridging Panel. Issued 1995
US Patent # 5414944 Splitter Plate Vortex Generators. Issued 1995
American Institute of Aeronautics & Astronautics member
AIAA Carolina Section,
Chairman 1985 - 1989
Secretary-Treasurer 1981-1984
Acoustical Society of America
Vice Chair, NC regional Section 1996- present
Chair, NC regional Section 1993
Vice Chair, NC regional Section 1990
Reviewer for NSF 1995-2001
Reviewer for ASME 1988-97
Reviewer for Journal of Fluid Mechanics 1982-1991
Reviewer for National Research Council 1986-1989
Reviewer for AIAA Journal 1987-present
Mentor in NCSSM Mentor program 1983-84, 1986-88