'Load case' presentation slideshows

Prof. P. M. Mujumdar, Prof. K. Sudhakar H. C. Ajmera, S. N. Abhyankar, M. Bhatia

WingOpt - An MDO Tool for Concurrent Aerodynamic Shape and Structural Sizing Optimization of Flexible Aircraft Wings. Prof. P. M. Mujumdar, Prof. K. Sudhakar H. C. Ajmera, S. N. Abhyankar, M. Bhatia Dept. of Aerospace Engineering, IIT Bombay. Develop a software for MDO of aircraft wing

922 views • 80 slides

AERSP 301 Fall 2008

AERSP 301 Fall 2008. Introduction to Flight Vehicle Structures. Jose L. Palacios. The Pennsylvania State University Department of Aerospace Engineering August 2008. Syllabus. Course Objectives Students who successfully complete this course will be able to:

1.13k views • 73 slides

The Mechanical Behavior of Orbital Fat in a Finite Element Model of Orbital Mechanics

The Mechanical Behavior of Orbital Fat in a Finite Element Model of Orbital Mechanics. by Frans-Willem Goudsmit. Human eye movement. To view objects when the head is moving Gaze towards new object of interest that pop up Maintaining gaze on interesting objects Follow objects as they move.

636 views • 49 slides

National Wind Technology Center

Wind Turbine Design According to IEC 61400-1 (Onshore) and -3 (Offshore) Standards Overview for NWTC November 8 , 2005 Sandy Butterfield NREL. National Wind Technology Center. Outline. Overview of design process IEC standards organization Load cases Determination of design load

476 views • 28 slides

10 - examples

354 views • 27 slides

Estimated Time for Completion: 30 minutes Experience Level: Lower

Compliant Stroke Amplifier. MSC.Marc 2005r2 MSC.Patran 2005r2. Estimated Time for Completion: 30 minutes Experience Level: Lower. Topics Covered. Using beam elements Creating non-spatial field Mapping function to tabular field Creating time-dependent boundary condition

362 views • 26 slides

573 views • 15 slides

Optimality criterion methods

Optimality criterion methods. Methods that use directly an optimality criterion in order to resize the structure. Fully stress design and stress ratio resizing. Dual methods. Simple resizing rule based on Lagrange multiplier for single constraint. Fully stressed design.

463 views • 10 slides

Analysis of Coil Structures Integrated Modular, TF and PF Modeling

Analysis of Coil Structures Integrated Modular, TF and PF Modeling. Work by HM Fan. Status. Modeling of Integrated Structure Completed and debugged Mostly Linear except for Wing Interfaces Runs on existing 32 bit, 2GB computer platforms in ~ 14 hrs Four load cases run so far:

187 views • 6 slides

Design, Manufacture, Transport and Integration on-site in Chile of ALMA Antennas PM#5

Design, Manufacture, Transport and Integration on-site in Chile of ALMA Antennas PM#5 Design and Engineering Toulose 21-22 June 2006. ENGINEERING AND DESIGN ACTIVITIES Technical meeting with Partners to review the design of the industrialization process of the following items:

235 views • 6 slides