High-Speed Wind-Tunnel Tests of a 1/6-scale Model of a Twin-Engine Pursuit Airplane

Open PDF

Document Details

Document Type
Technical Report
Publication Date
Dec 01, 1942
Accession Number
ADA800811

Entities

People

  • Victor M. Ganzer

Organizations

  • National Aeronautics and Space Administration

Tags

DTIC Thesaurus Topics

  • Aeronautical Laboratories
  • Aeronautics
  • Aircrafts
  • Airplanes
  • Coefficients
  • Flight
  • Flow
  • Fuselages
  • Level Flight
  • Mach Number
  • Measurement
  • Models
  • Oil Coolers
  • Pressure Distribution
  • Reynolds Number
  • Wind Tunnel Tests
  • Wind Tunnels