UT Arlington
  Home >  MAE Faculty Index > Seath

MAE A - Z Index

D. D. Seath, Ph.D.
Professor and A.E. Undergraduate Advisor

Education: Ph.D. Iowa State University, 1963 ~ M.S.A.E. Iowa State University, 1959 ~ B.S.A.E. Iowa State University, 1954

Areas of Expertise: Low-speed aerodynamic analysis and wind tunnel testing, stability and control and performance analysis of flight vehicles, wing (and body) vortex interaction effects, conceptual aircraft design, and wind energy conversion systems rotor analysis and testing.

Background: Dr. Seath has had industrial experience at General Dynamics (1963-1965) in low-speed vortex lift analysis of low-aspect-ratio wings and conformal transformation of arbitrary airfoils. He was also involved in development of a mesh geometry for finite difference analysis of flows about airfoils. He served in the United States Air Force as a Jet Fighter Pilot (1954-1957). He was an Instructor in Aerospace Engineering at Iowa State University (1959-1963). He joined UT Arlington in 1965. He has teaching experience in aerodynamics of wings and bodies, flight mechanics, potential flow analysis, fluid mechanics, wind tunnel testing, astronautics, hydronautics, nuclear reactor design, aerospace vehicle design, engineering mechanics-statics and dynamics. He did consulting work in anemometer calibration (Ceramic Cooling Tower Company), airspeed system calibration (STOL Aircraft Company), performance prediction for high lift on aircraft (Wren Aircraft Company), prediction of low-speed aerodynamic characteristics of hypersonic vehicles (USAF Flight Dynamics Lab), and wind tunnel tests of pedestal mounted heliostats (Northrup Incorporated). Also, consulting work was done on the analysis of wind energy conversion systems (Standard Manufacturing and STL Corp.), axial flow fan design (Behlen Corporation), analysis of an aircraft onboard aerodynamic measurement system (Precision Aerodynamics), wind tunnel testing and analysis of broadcast tower pod configurations (Landmark Tower Corp.), and wind tunnel testing and analysis of flying disks (Glaser, Griggs, & Schwartz).

E-mail: seath@uta.edu

©2006 Mechanical and Aerospace Engineering at The University of Texas at Arlington
500 West First Street, 211 Woolf Hall, Arlington, TX 76019-0018