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Carlos Eduardo Cesnik

from Ann Arbor, MI
Age ~61
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Also known as:
Carlos E Cesnik, Carlos E Cesnick, Cibele Cesnik, Cesnik Cibele
Phone and address:
3248 Bellflower Ct, Ann Arbor, MI 48103
(734) 214-3994
Related to:
Brandon C Doyle, 48
Connected to:
Carol A Cesnik, 59Amaury Cespedes, 52Andres Cespedes, 86Antonio Cespedes, 45Ariel Q Cespedes, 64Beatriz Cespedes, 66Blanca M Cespedes, 54Brian Cespedes, 41Carlos A Cespedes, 70Catalina R Cespedes, 65

Carlos Cesnik Phones & Addresses

  • 3248 Bellflower Ct, Scio Township, MI 48103 (734) 214-3994
  • 3248 Bellflower Ct APT 74, Ann Arbor, MI 48103 (734) 620-3042
  • Atlanta, GA
  • 91 Channing Rd, Watertown, MA 02472 (617) 924-8316
  • Fort Lauderdale, FL

Work

Company: University of michigan Mar 2019 Position: Clarence l â kellyâ johnson professor of aerospace engineering

Education

Degree: Doctorates, Doctor of Philosophy School / High School: Georgia Institute of Technology 1989 to 1994 Specialities: Engineering, Philosophy

Skills

Aerospace Engineering • Aerospace • Aeronautics • Finite Element Analysis • Simulations • Matlab • Fortran • Cfd • Engineering • Aerodynamics • Numerical Analysis • Structural Dynamics • Composites • Mathematical Modeling • Systems Engineering • Mathematica • Simulink • Aircraft • Aeroelasticity • Fluid Dynamics • Fluid Mechanics • Engineering Management • Higher Education • Ansys • Labview • Dynamics • Modeling • Solidworks • Optimization • Structural Analysis • Catia • Stress Analysis • Sensors • Space Systems • Numerical Simulation • Computational Fluid Dynamics • Aviation

Languages

Portuguese • English • Spanish

Industries

Higher Education

Resumes

Resumes

Carlos Cesnik Photo 1

Director, Aerospace Design And Structures Group

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Location:
Detroit, MI
Industry:
Higher Education
Work:
University of Michigan
Clarence L Â Kellyâ Johnson Professor of Aerospace Engineering
Aiaa
Director, Aerospace Design and Structures Group
Aiaa 2009 - 2014
Deputy Director, Aerospace Design and Structures Group
Ahs 1989 - 2013
Member
Nato Rto 2005 - 2012
Member
Education:
Georgia Institute of Technology 1989 - 1994
Doctorates, Doctor of Philosophy, Engineering, Philosophy Instituto Tecnológico De Aeronáutica - Ita 1983 - 1987
Skills:
Aerospace Engineering
Aerospace
Aeronautics
Finite Element Analysis
Simulations
Matlab
Fortran
Cfd
Engineering
Aerodynamics
Numerical Analysis
Structural Dynamics
Composites
Mathematical Modeling
Systems Engineering
Mathematica
Simulink
Aircraft
Aeroelasticity
Fluid Dynamics
Fluid Mechanics
Engineering Management
Higher Education
Ansys
Labview
Dynamics
Modeling
Solidworks
Optimization
Structural Analysis
Catia
Stress Analysis
Sensors
Space Systems
Numerical Simulation
Computational Fluid Dynamics
Aviation
Languages:
Portuguese
English
Spanish

Publications

Wikipedia References

Carlos Cesnik Photo 2

Carlos Cesnik

Us Patents

High-G Compact Folding Wing

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US Patent:
62607987, Jul 17, 2001
Filed:
Oct 22, 1999
Appl. No.:
9/425609
Inventors:
Thierry Casiez - Montreal, CA
Carlos Cesnik - Watertown MA
Mark Drela - Cambridge MA
Staci N. Jenkins - Santa Clara CA
Mark Spearing - Newton MA
Assignee:
Massachusetts Institute of Technology - Cambridge MA
International Classification:
B64C 338
US Classification:
244 49
Abstract:
A compact, aerodynamic wing assembly constructed and arranged so as to withstand a force due to acceleration in at least one direction includes at least two wing segments, each of the wing segments having a span-wise axis, and a airfoil cross section normal to the span axis. The wing segments are preferably disposed mutually adjacent and end to end. For each pair of wing segments, the wing further includes a pivot assembly fixedly attached to the wing segments at an end of each of the wing segments along the span-wise axis. The pivot assembly forms an articulation axis for relative movement between each the pair of wing segments, such that the wing assembly converts, upon a predetermined stimulus, from a stowed configuration characterized by nested wing segments, to a deployed configuration characterized by a substantially uninterrupted aerodynamic surface. The wing assembly is preferably constructed and arranged to withstand forces due to acceleration in at least two directions, including 15,000 g's forward and 4,000 g's rebound accelerations. The invention further comprises a flying structure constructed and arranged so as to withstand an acceleration force directed along a main axis.
Control profile
Carlos Eduardo Cesnik from Ann Arbor, MI, age ~61 Get Report