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Trailing-Edge Flap Placement

  • Ranjan GanguliEmail author
  • Dipali Thakkar
  • Sathyamangalam Ramanarayanan Viswamurthy
Chapter
  • 1.4k Downloads
Part of the Advances in Industrial Control book series (AIC)

Abstract

The optimal location of flaps for multiple-flap configuration shown in Chap.  4 was obtained through parametric studies and the objective was to minimize only the hub vibration levels. These trailing-edge flaps are typically operated using piezoceramic actuators placed inside the blade section.

Keywords

Response Surface Response Surface Methodology Central Composite Design Design Point Pareto Point 
These keywords were added by machine and not by the authors. This process is experimental and the keywords may be updated as the learning algorithm improves.

References

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    Viswamurthy, S.R., Ganguli, R.: Optimal placement of trailing-edge flaps for helicopter vibration reduction using response surface methods. Eng. Optim. 39(2), 185–202 (2007)Google Scholar

Copyright information

© Springer International Publishing Switzerland 2016

Authors and Affiliations

  • Ranjan Ganguli
    • 1
    Email author
  • Dipali Thakkar
    • 2
  • Sathyamangalam Ramanarayanan Viswamurthy
    • 3
  1. 1.Department of Aerospace EngineeringIndian Institute of ScienceBangaloreIndia
  2. 2.Department of Aeronautical EngineeringSardar Vallabhbhai Patel Institute of TechnologyVasadIndia
  3. 3.Advanced Composites DivisionCSIR-National Aerospace LaboratoriesBangaloreIndia

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