System Modification Data. Modification of T-39 NLG Drawings and Analyses. Reference Contract Item 0002, Data Item A003,

Abstract

The report contains the Static and Fatigue Stress Analysis and supplementary engineering data required to support the design changes for modification of the T-39 Nose Landing Gear Assembly.

Document Details

Document Type
Technical Report
Publication Date
Mar 27, 1972
Accession Number
ADA008651

Entities

People

  • C. Y. Chu

Tags

DTIC Thesaurus Topics

  • Assembly
  • Contracts
  • Engineering
  • Landing Gear
  • Stress Analysis
  • Stresses

Readers

  • Aerospace Engineering
  • Software Engineering