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Saeed Farokhi Phones & Addresses

  • 1270 Cleveland Ave #217, San Diego, CA 92103 (619) 295-9811
  • 1270 Cleveland Ave, San Diego, CA 92103
  • 5706 Villa Dr, Laurence, KS 66047 (785) 856-3095 (785) 856-4395
  • 3115 6Th St, Laurence, KS 66049 (785) 865-5027
  • 3125 W 6Th St, Laurence, KS 66049 (785) 865-5027
  • Lawrence, KS
  • 3 Sorbonne, Laguna Niguel, CA 92677 (949) 276-4849
  • Orange, CA

Resumes

Resumes

Saeed Farokhi Photo 1

Assiciate Dean Of The Graduate School , Professor Of Associate Editor

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Location:
San Diego, CA
Industry:
Higher Education
Work:
The University of Kansas
Assiciate Dean of the Graduate School , Professor of Associate Editor
Skills:
Research
Teaching
Matlab
Higher Education
Science
Microsoft Office
Curriculum Design
Public Speaking
College Teaching
University Teaching
Microsoft Word
Programming
Experimentation
Technical Writing
Powerpoint
Statistics
Aerodynamics
Educational Leadership
Mathematical Modeling
Microsoft Excel
Simulations
Project Management
Numerical Analysis
Student Affairs
Fortran
Tutoring
Leadership
Faculty Development
Labview
Social Networking
Event Planning
Staff Development
Adult Education
Customer Service
C++
Distance Learning
Finite Element Analysis
Student Development
Curriculum Development
Strategic Planning
Academic Advising
Photoshop
Event Management
Strategic Communications
Program Management
Team Building
Latex
English
Visual Basic
Coaching
Saeed Farokhi Photo 2

Saeed Farokhi

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Publications

Us Patents

Supersonic Vortex Generator

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US Patent:
55989900, Feb 4, 1997
Filed:
Dec 15, 1994
Appl. No.:
8/356646
Inventors:
Saeed Farokhi - Lawrence KS
Ray R. Taghavi - Lawrence KS
Assignee:
University of Kansas Center for Research Inc. - Lawrence KS
International Classification:
B64C 2306
US Classification:
244199
Abstract:
A vortex generator for attenuating flow separation which occur during supersonic flow of air over structure such as an aircraft airfoil, its fuselage, surfaces forming a part of a jet propulsion unit, turbine or compressor blades, or similar surfaces subjected to supersonic airflow. A series of vortex generators are provided each of which comprises a cavity in the component over which the supersonic air is flowing that is configured to generate a spiral vortex which attenuates flow separation and weight drag resulting from the supersonic airflow. Each cavity is of generally triangular configuration defined by two side walls which diverge in a direction away from the apex of the triangular cavity, and a flat bottom wall joined to the side walls. In an alternate embodiment, means is provided for selectively shifting the bottom wall from a retracted inner position, to an outer location essentially flush with the surface over which the supersonic airflow is occurring.
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