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Lakshmi N Sankar, 741217 Empire Rd NE, Atlanta, GA 30329

Known as:
Lakshmi Dr Sankar Lakshmi Pramon Sankar Laksemi Sankar Sankar N Lakshmi
Related to:
Lisa J Sankar 39

Lakshmi Sankar Phones & Addresses

1217 Empire Rd NE, Atlanta, GA 30329    404-6339966   

Tucker, GA   

Stone Mountain, GA   

1217 Empire Rd NE, Atlanta, GA 30329   

Work

Position: Production Occupations

Education

Degree: Bachelor's degree or higher

Emails

d***[email protected]
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Lakshmi Sankar resumes & CV records

Resumes

Lakshmi Sankar Photo 23

Regents Professor And Sikorsky Professor

Location:
Atlanta, GA
Industry:
Higher Education
Work:
Georgia Institute of Technology
Regents Professor and Sikorsky Professor Lockheed Martin Apr 1979 - Jun 1982
Scientist Associate School of Aerospace Engineering Georgia Tech Apr 1979 - Jun 1982
Regents Professor and Associate Chair Georgia Institute of Technology Apr 1979 - Jun 1982
Regents Professor
Education:
Georgia Institute of Technology 1973 - 1977
Indian Institute of Technology, Madras 1968 - 1973
Bachelors, Bachelor of Technology, Engineering
Skills:
Cfd, Fluid Mechanics, Aerodynamics, Fortran, Matlab, Simulations, Fluid Dynamics, Aerospace Engineering, Numerical Analysis, Research, Heat Transfer, Microsoft Office, Thermodynamics, Tecplot, Turbulence, Ansys, Mathematica, Engineering, Finite Element Analysis, Simulink, Fluids, Computational Fluid Dynamics, Turbomachinery, Mathematical Modeling, Latex, Fieldview, Openfoam, Experimentation, Numerical Simulation, Composites, Aircraft Design, Propulsion, Abaqus, Comsol, Computational Mechanics, Dynamics, Structural Analysis
Lakshmi Sankar Photo 24

Lakshmi Sankar

Publications & IP owners

Us Patents

Blade Vortex Interaction Noise Reduction Techniques For A Rotorcraft

US Patent:
5711651, Jan 27, 1998
Filed:
Jun 13, 1996
Appl. No.:
8/662601
Inventors:
Bruce D. Charles - Mesa AZ
Ahmed A. Hassan - Mesa AZ
Hormoz Tadghighi - Gilbert AZ
Ram D. JanakiRam - Mesa AZ
Lakshmi N. Sankar - Atlanta GA
Assignee:
McDonnell Douglas Helicopter Company - Mesa AZ
International Classification:
F01D 500
US Classification:
416 24
Abstract:
An active control device for reducing blade-vortex interactions (BVI) noise generated by a rotorcraft, such as a helicopter, comprises a trailing edge flap located near the tip of each of the rotorcraft's rotor blades. The flap may be actuated in any conventional way, and is scheduled to be actuated to a deflected position during rotation of the rotor blade through predetermined regions of the rotor azimuth, and is further scheduled to be actuated to a retracted position through the remaining regions of the rotor azimuth. Through the careful azimuth-dependent deployment and retraction of the flap over the rotor disk, blade tip vortices which are the primary source for BVI noise are (a) made weaker and (b) pushed farther away from the rotor disk (that is, larger blade-vortex separation distances are achieved).

Blade Vortex Interaction Noise Reduction Techniques For A Rotorcraft

US Patent:
5588800, Dec 31, 1996
Filed:
May 31, 1994
Appl. No.:
8/251329
Inventors:
Bruce D. Charles - Mesa AZ
Ahmed A. Hassan - Mesa AZ
Hormoz Tadghighi - Gilbert AZ
Ram D. JanakiRam - Mesa AZ
Lakshmi N. Sankar - Atlanta GA
Assignee:
McDonnell Douglas Helicopter Co. - Mesa AZ
International Classification:
F01D 500
US Classification:
416 24
Abstract:
An active control device for reducing blade-vortex interactions (BVI) noise generated by a rotorcraft, such as a helicopter, comprises a trailing edge flap located near the tip of each of the rotorcraft's rotor blades. The flap may be actuated in any conventional way, and is scheduled to be actuated to a deflected position during rotation of the rotor blade through predetermined regions of the rotor azimuth, and is further scheduled to be actuated to a retracted position through the remaining regions of the rotor azimuth. Through the careful azimuth-dependent deployment and retraction of the flap over the rotor disk, blade tip vortices which are the primary source for BVI noise are (a) made weaker and (b) pushed farther away from the rotor disk (that is, larger blade-vortex separation distances are achieved).

Possible Relatives

David Sankar  Govindasamy Sankar  Krishna Sankar  Malini Sankar  Maria V Sankar  Nalini N Sankar  Narendra N Sankar  Lakshmi P Nair  Lakshmi W Singh  Lakshmi Das 

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