A COMPARISON OF THE CALCULATED AND OBSERVED FLUTTER CHARACTERISTICS OF A HELICOPTER ROTOR BLADE HAVING BOTH CONTROL SYSTEM AND BLADE FLEXIBILITY

Document Details

Document Type
Technical Report
Publication Date
Dec 01, 1955
Accession Number
AD0083965

Entities

People

  • A.a. Perlmutter
  • Leonard Goland

Organizations

  • Princeton University

Tags

DTIC Thesaurus Topics

  • Aircrafts
  • Airframes
  • Control Systems
  • Helicopter Rotors
  • Helicopters
  • Resilience
  • Rotary Wing Aircraft
  • Vehicles