INVESTIGATION AT HIGH SUBSONIC SPEEDS OF THE EFFECT OF HORIZONTAL-TAIL LOCATION ON LONGITUDINAL AND LATERAL STABILITY CHARACTERISTICS OF A COMPLETE MODEL HAVING A SWEPTBACK WING IN A HIGH LOCATION

Open PDF

Document Details

Document Type
Technical Report
Publication Date
Apr 18, 1956
Accession Number
AD0091844

Entities

People

  • H. N. Silvers
  • Thomas J. King Jr.

Organizations

  • Langley Research Center

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Aerodynamic Characteristics
  • Aerodynamic Configurations
  • Aeronautical Laboratories
  • Aircrafts
  • Dynamic Pressure
  • Government Procurement
  • Governments
  • Horizontal Stabilizers
  • Mach Number
  • National Security
  • Reynolds Number
  • Static Pressure
  • Sweptback Wings
  • Tail Assemblies
  • United States
  • United States Government
  • Wind Tunnels