Aerodynamic Characteristics of a Wing with Unswept Quarter-Chord Line, Aspect Ratio 4, Taper Ratio 0.6, and NACA 65A004 Airfoil Section - Transonic-Bump Method

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Document Details

Document Type
Technical Report
Publication Date
May 08, 1950
Accession Number
ADA801299

Entities

People

  • Boyd C. Myers Ii
  • James W. Wiggins

Organizations

  • Langley Research Center

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Aerodynamic Characteristics
  • Aeronautical Laboratories
  • Aeronautics
  • Aspect Ratio
  • Bending Moments
  • Boundaries
  • Boundary Layer
  • Drag
  • Dynamic Pressure
  • Fineness Ratio
  • Flow
  • Flow Fields
  • Free Stream
  • Geometry
  • Mach Number
  • Reynolds Number
  • Static Pressure