Accession Number:

ADA222543

Title:

Rotorcraft Aeromechanical Stability-Methodology Assessment. Phase 2. Workshop

Descriptive Note:

Technical memo.

Corporate Author:

NATIONAL AERONAUTICS AND SPACE ADMINISTRATION MOFFETT FIELD CA AMES RESEARCHCENTER

Personal Author(s):

Report Date:

1990-03-01

Pagination or Media Count:

269.0

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

Subject Categories:

  • Aerodynamics
  • Helicopters

Distribution Statement:

APPROVED FOR PUBLIC RELEASE