AERO ELASTIC EFFECTS ON THE STABILITY AND CONTROL OF AIRCRAFT DESIGNED TO OPERATE AT MACH NUMBERS UP TO 2.5

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Document Details

Document Type
Technical Report
Publication Date
Nov 01, 1955
Accession Number
AD0091759

Entities

People

  • A. S. Taylor
  • K. W. James

Organizations

  • Royal Aircraft Establishment

Tags

DTIC Thesaurus Topics

  • Aerodynamic Configurations
  • Aircraft Equipment
  • Aircrafts
  • Airframes
  • Airplanes
  • Aspect Ratio
  • Control Surfaces
  • Control Systems
  • Delta Wings
  • Digital Computers
  • Flaps (Control Surfaces)
  • Government Procurement
  • Governments
  • Mach Number
  • Supersonic Aircraft
  • Swept Wings
  • Trailing Edges