Subsonic Longitudinal Aerodynamic Measurements on a Transport Model in Two Slotted Tunnels Differing in Size

Abstract

The investigations were made in the Langley 8-foot transonic pressure tunnel and in the Langley 16-foot transonic tunnel.

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Document Details

Document Type
Technical Report
Publication Date
Oct 01, 1968
Accession Number
ADA279177

Entities

People

  • Arvo A. Luoma
  • Donald L. Loving
  • Richard J. Re

Organizations

  • National Aeronautics and Space Administration

Tags

Communities of Interest

  • Air Platforms
  • Autonomy
  • Weapons Technologies

DTIC Thesaurus Topics

  • Accuracy
  • Aerodynamic Characteristics
  • Aerodynamic Configurations
  • Aerodynamic Forces
  • Aircrafts
  • Airfoils
  • Boundary Layer
  • Flow
  • Fuselages
  • Geometry
  • Horizontal Stabilizers
  • Mach Number
  • Measurement
  • Polyethylene Glycols
  • Reynolds Number
  • Strain Gages
  • Wind Tunnels

Fields of Study

  • Physics

Readers

  • Aerodynamics/Aeronautics.