Aerodynamic Characteristics of a Wing with Unswept Quarter-Chord Line, Aspect Ratio 2, Taper Ratio 0.78, and NACA 65A004 Airfoil Section - Transonic Bump Method

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Document Details

Document Type
Technical Report
Publication Date
Mar 08, 1950
Accession Number
ADA801172

Entities

People

  • Edward C. Polhamus
  • George S. Campbell

Organizations

  • Langley Research Center

Tags

DTIC Thesaurus Topics

  • Abstracts
  • Aerodynamic Characteristics
  • Aeronautical Laboratories
  • Aeronautics
  • Air Force
  • Air Force Facilities
  • Airfoils
  • Aspect Ratio
  • Bending Moments
  • Boundaries
  • Boundary Layer
  • Flow Fields
  • Free Stream
  • Leading Edges
  • Mach Number
  • Mechanical Properties
  • Military Organizations