EFFECTS OF SPOILER AILERONS ON THE AERODYNAMIC LOAD DISTRIBUTION OVER A 45 SWEPTBACK WING AT MACH NUMBERS FROM 0.60 TO 1.03

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Document Details

Document Type
Technical Report
Publication Date
May 14, 1954
Accession Number
AD0030433

Entities

People

  • F. E. West Jr.
  • George Liner
  • Joseph M. Hallissy Jr.

Organizations

  • National Aeronautics and Space Administration

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Aerodynamic Configurations
  • Flow
  • Flow Separation
  • High Angles
  • Leading Edges
  • Load Distribution
  • Low Angles
  • Mach Number
  • Measurement
  • Pressure Distribution
  • Pressure Measurement
  • Reynolds Number
  • Spoilers
  • Static Pressure
  • Swept Wings
  • Sweptback Wings
  • Trailing Edges