THE EFFECT OF MACH NUMBER AND LIFT COEFFICIENT ON THE DIRECTIONAL STABILITY, DIHEDRAL EFFECT AND SIDE-FORCE DERIVATIVE OF A SWEPT-WING JET FIGHTER

Document Details

Document Type
Technical Report
Publication Date
May 15, 1958
Accession Number
AD0162656

Entities

People

  • John H. Craigie

Organizations

  • Princeton University

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Aircraft Wings
  • Airfoils
  • Airframes
  • Coefficients
  • Directional
  • Mach Number
  • Swept Wings