Fatigue Test of OH-58A Main Rotor Blade (P. I. P. Task No. 69-6).

Abstract

A fatigue test of a main helicopter rotor blade assembly was conducted as part of a product improvement program to increase the service life of the blade from the existing 1200 hours. Results are reported. (Author)

Document Details

Document Type
Technical Report
Publication Date
Jul 01, 1971
Accession Number
AD0746983

Entities

People

  • I. L. Reese

Tags

DTIC Thesaurus Topics

  • Aircrafts
  • Airframes
  • Assembly
  • Fatigue Tests (Mechanics)
  • Helicopter Rotors
  • Helicopters
  • Rotary Wing Aircraft
  • Vehicles

Fields of Study

  • Physics

Readers

  • Aerospace Engineering
  • Software Engineering
  • Structural Health Monitoring of Composite Structures.