FREE-FLIGHT INVESTIGATION OF THE CONTROL EFFECTIVENESS OF A DIFFERENTIALLY DEFLECTED HORIZONTAL TAIL AT MACH NUMBERS FROM 0.8 TO 1.6

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Document Details

Document Type
Technical Report
Publication Date
Apr 26, 1956
Accession Number
AD0092212

Entities

People

  • A. James Vitale
  • Jesse L. Mitchell

Organizations

  • Langley Research Center

Tags

Communities of Interest

  • Weapons Technologies

DTIC Thesaurus Topics

  • Aerodynamic Characteristics
  • Aerodynamic Configurations
  • Aeroelasticity
  • Aeronautical Laboratories
  • Aircrafts
  • Airplanes
  • Delta Wings
  • Flight
  • Free Flight
  • Government Procurement
  • Horizontal Stabilizers
  • Mach Number
  • Stabilization Systems
  • Sweptback Wings
  • Unmanned Aerial Vehicles
  • Wind Tunnel Tests
  • Wind Tunnels