Optimum design of high speed proprotors using a multidisciplinary approach

Aditi Chattopadhyay, Johnny R. Narayan

Research output: Contribution to journalArticle

10 Scopus citations

Abstract

The design of advanced high speed proprotor aircraft is addressed using a formal multidisciplinary optimization procedure. The optimization problem is formulated with aerodynamic performance, dynamics, aeroelastic stability and structural design requirements. Both high speed cruise and hover flight conditions are addressed. The analysis is performed at a cruise speed of 400 knots. The efficiency in cruise is maximized without deteriorating hover performance. Constraints are imposed on fundamental frequency, blade weight, thrust in hover, total power required and aeroelastic stability in cruise. A wide selection of structural and aerodynamic design variables are used. The optimization is performed using a nonlinear programming procedure and an approximate analysis technique. The procedure yields significant improvements in the overall rotor performance.

Original languageEnglish (US)
Pages (from-to)1-17
Number of pages17
JournalEngineering Optimization
Volume22
Issue number1
DOIs
StatePublished - Nov 1 1993

Keywords

  • aeroelastic stability
  • high speed proprotor
  • multidisciplinary optimization
  • performance
  • tilt rotor

ASJC Scopus subject areas

  • Computer Science Applications
  • Control and Optimization
  • Management Science and Operations Research
  • Industrial and Manufacturing Engineering
  • Applied Mathematics

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