STRUCTURAL TEST PROGRAM F-106A AIRPLANE

Abstract

The F-106 airplane was subjected to a complete static test program covering all of the critical flight, landing and ground handling conditions.

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Document Details

Document Type
Technical Report
Publication Date
Aug 01, 1960
Accession Number
AD0249771

Entities

People

  • David W. Jackson
  • Fred E. Hussong
  • Sanford Lustig

Tags

Communities of Interest

  • Air Platforms
  • Weapons Technologies

DTIC Thesaurus Topics

  • Air Force
  • Aircrafts
  • Airframes
  • Boundary Layer
  • Engine Mounts
  • Engineering
  • Fuselages
  • Heat Flux
  • Heat Transfer
  • Heat Transfer Coefficients
  • Landing Gear
  • Leading Edges
  • Pilot Seats
  • Simulations
  • Spars
  • Test And Evaluation
  • Test Facilities