WIND-TUNNEL INVESTIGATION OF A RAM-JET MISSILE MODEL HAVING A WING AND CANARD SURFACES OF DELTA PLAN FORM WITH 70 SWEPT LEADING EDGES. FORCE AND MOMENT CHARACTERISTICS AT COMBINED ANGLES OF PITCH AND SIDESLIP FOR MACH NUMBER 2.01

Open PDF

Document Details

Document Type
Technical Report
Publication Date
Apr 26, 1956
Accession Number
AD0092213

Entities

People

  • Clyde V. Hamilton
  • Cornelius Driver

Organizations

  • Langley Research Center

Tags

Communities of Interest

  • Air Platforms
  • Weapons Technologies

DTIC Thesaurus Topics

  • Aerodynamic Characteristics
  • Aeronautical Laboratories
  • Aircrafts
  • Base Pressure
  • Bodies
  • Canard Configurations
  • Center Of Gravity
  • Drag
  • Dynamic Pressure
  • Flow
  • Government Procurement
  • Governments
  • Leading Edges
  • Mach Number
  • Measurement
  • Pressure Measurement
  • Reynolds Number