HEAVY-LIFT TIP TURBOJET ROTOR SYSTEM. VOLUME 7. WEIGHT AND BALANCE STUDIES

Abstract

The report discusses statistical, analytical, and empirical weight analysis methods used to evaluate the empty weight of the helicopter. Blade lag characteristics are also discussed, including an analysis showing blade lag angles with one and two engines inoperative. Included are aircraft balance predictions.

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Document Details

Document Type
Technical Report
Publication Date
Oct 01, 1965
Accession Number
AD0624813

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Abstracts
  • Aircrafts
  • Center Of Gravity
  • Centrifugal Force
  • Classification
  • Electronics
  • Engines
  • Fuel Systems
  • Generators
  • Governments
  • Helicopters
  • Identification Systems
  • Jet Aircraft
  • Leading Edges
  • Pressure Gages
  • Security
  • Trailing Edges

Fields of Study

  • Physics

Readers

  • Aerospace Engineering
  • Computational Modeling and Simulation