PHASE IV PERFORMANCE TEST OF THE F-86F-40 AIRPLANE EQUIPPED WITH 6 X 3-INCH LEADING EDGE SLATS AND 12-INCH EXTENSIONS ON THE WING TIPS

Open PDF

Document Details

Document Type
Technical Report
Publication Date
May 01, 1956
Accession Number
AD0096084

Entities

People

  • Norris J. Hanks

Organizations

  • Air Force Test Center

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Air Force
  • Air Force Facilities
  • Aircrafts
  • Airfoils
  • Airplanes
  • Altitude
  • Aspect Ratio
  • Horizontal Stabilizers
  • Indicators
  • Instrumentation
  • Intact Stability
  • Leading Edges
  • Level Flight
  • Mach Number
  • Performance Tests
  • United States
  • Wing Tips