HEAVY-LIFT TIP TURBOJET ROTOR SYSTEM. VOLUME 5. STRUCTURAL ANALYSIS

Abstract

The report discusses stress calculations for major structural components of this system. Tip engine attachment hardware is also analyzed.

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Document Details

Document Type
Technical Report
Publication Date
Oct 01, 1965
Accession Number
AD0625820

Tags

Communities of Interest

  • Ground and Sea Platforms

DTIC Thesaurus Topics

  • Abstracts
  • Aircrafts
  • Attachment
  • Bending Moments
  • Bending Stress
  • Engines
  • Geometry
  • Jet Aircraft
  • Margin Of Safety
  • Modulus Of Elasticity
  • Shear Stresses
  • Stress Analysis
  • Structural Analysis
  • Structural Components
  • Tensile Stress
  • Titanium Alloys
  • Turbojet Engines

Fields of Study

  • Physics

Readers

  • Aerospace Engineering