Preliminary Investigation of Spoiler Lateral Control on a 42 deg Sweptback Wing at Transonic Speeds

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Document Details

Document Type
Technical Report
Publication Date
Aug 12, 1947
Accession Number
ADA800752

Entities

People

  • Howard L. Ziff
  • Leslie E. Schneiter

Organizations

  • Langley Research Center

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Aeronautical Laboratories
  • Aeronautics
  • Aircrafts
  • Airfoils
  • Aspect Ratio
  • Barometric Pressure
  • Boundary Layer
  • Boundary Layer Flow
  • Control Systems
  • Dynamic Pressure
  • Flow
  • Flow Fields
  • Leading Edges
  • Mach Number
  • Pressure Distribution
  • Sweptback Wings
  • Trailing Edges