HEAVY-LIFT TURBOJET ROTOR SYSTEM. VOLUME 4. STATIC AND DYNAMIC LOADS

Abstract

The report presents the structural design criteria, static design loads, and dynamic design loads for the Model 1108 helicopter. The volume is the basis for the structural design and analysis of the tip turbojet main rotor system.

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Document Details

Document Type
Technical Report
Publication Date
Oct 01, 1965
Accession Number
AD0624763

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Aerodynamic Characteristics
  • Aircrafts
  • Airframes
  • Analog Computers
  • Classification
  • Computer Simulations
  • Computers
  • Control Systems
  • Design Criteria
  • Digital Computers
  • Dynamic Loads
  • Engines
  • Flight Maneuvers
  • Governments
  • Mechanics
  • Turbine Components
  • Turbojet Engines

Fields of Study

  • Physics

Readers

  • Aerodynamics.