Rotorcraft Aeromechanical Stability-Methodology Assessment. Phase 2. Workshop

Abstract

Helicopter rotor aeroelastic and aeromechanical stability predictions for four data sets were made using industry and government stability analyses and compared with data at a workshop held at Ames Research Center, August 2-3, 1988. The present report contains the workshop comparisons. Keywords: Aeromechanic stability; Rotary wing aircraft; Aeroelastic stability; Rotorcraft dynamics; Aerodynamic stability; Aeroelasticity; Helicopter rotors. (edc)

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Document Details

Document Type
Technical Report
Publication Date
Mar 01, 1990
Accession Number
ADA222543

Entities

People

  • William G. Bousman

Organizations

  • National Aeronautics and Space Administration

Tags

DTIC Thesaurus Topics

  • Aerodynamic Stability
  • Aircrafts
  • Airframes
  • Army Aviation
  • Coordinate Systems
  • Couplings
  • Data Sets
  • Experimental Data
  • Frequency
  • Helicopter Rotors
  • Helicopters
  • Hingeless
  • Model Tests
  • Rotary Wing Aircraft
  • Stiffness
  • Unsteady Aerodynamics
  • Workshops

Fields of Study

  • Physics

Readers

  • Academic Conference Management
  • Aerospace Engineering