LOW-SPEED INVESTIGATION OF THE EFFECTS OF WING DIHEDRAL ANGLE AND FIN LENGTH ON THE STATIC STABILITY CHARACTERISTICS OF A MODEL HAVING AN 82 DEG. DELTA WING

Open PDF

Document Details

Document Type
Technical Report
Publication Date
Apr 02, 1956
Accession Number
AD0092662

Entities

People

  • Kenneth P. Spreemann

Organizations

  • National Aeronautics and Space Administration

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Aerodynamic Configurations
  • Aeronautical Laboratories
  • Aircrafts
  • Bodies
  • Coefficients
  • Delta Wings
  • Dihedral Angle
  • Directional
  • Dynamic Pressure
  • Fineness Ratio
  • Government Procurement
  • Governments
  • High Angles
  • Leading Edges
  • Reynolds Number
  • Static Pressure
  • United States Government