Effect of Compressibility on the Distribution of Pressures over a Tapered Wing of NACA 230-Series Airfoil Sections

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Document Details

Document Type
Technical Report
Publication Date
Jul 01, 1947
Accession Number
ADB804053

Entities

People

  • E. O. Pearson Jr.

Organizations

  • Langley Research Center

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Aeronautical Laboratories
  • Aeronautics
  • Aircrafts
  • Aspect Ratio
  • Coefficients
  • Compressive Properties
  • Dynamic Pressure
  • Fighter Aircraft
  • Flow
  • Flow Separation
  • Free Stream
  • Load Distribution
  • Mach Number
  • Measurement
  • Pressure Distribution
  • Pressure Measurement
  • Static Pressure