Tests of Submerged Duct Installation on a Modified Fighter Airplane in the Ames 40- by 80-foot Wind Tunnel

Open PDF

Document Details

Document Type
Technical Report
Publication Date
Dec 11, 1947
Accession Number
ADA800890

Entities

People

  • Norman J. Martin

Organizations

  • National Aeronautics and Space Administration

Tags

DTIC Thesaurus Topics

  • Aeronautics
  • Air Flow
  • Aircrafts
  • Airplanes
  • Boundary Layer
  • Dynamic Pressure
  • Fighter Aircraft
  • Flow
  • Inlets
  • Leading Edges
  • Mach Number
  • Pressure Distribution
  • Pressure Gradients
  • Pressure Measurement
  • Static Pressure
  • Wind Tunnels
  • Wing Inlets