Flight Investigation of the Variation of Static-Pressure Error of a Static-Pressure Tube With Distance Ahead of a Wing and a Fuselage

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Document Details

Document Type
Technical Report
Publication Date
Mar 01, 1951
Accession Number
ADA382270

Entities

People

  • Elwood F. Scheithauer
  • William Gracey

Organizations

  • National Aeronautics and Space Administration

Tags

DTIC Thesaurus Topics

  • Aeronautical Laboratories
  • Aeronautics
  • Aircrafts
  • Airplanes
  • Bodies
  • Fighter Aircraft
  • Fineness Ratio
  • Fuselages
  • Leading Edges
  • Mach Number
  • Models
  • Shape
  • Static Pressure
  • Wind Tunnel Models
  • Wind Tunnel Tests
  • Wind Tunnels
  • Wing Tips