Free-Flight Investigation at Supersonic Speeds of the Stability and Drag of a 79 deg Clipped Delta Boost-Glide Configuration Including an Analog Study of Coupled Motions during the Flight

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Document Details

Document Type
Technical Report
Publication Date
Jan 01, 1961
Accession Number
AD0223723

Entities

People

  • Sherwood Hoffman
  • Willard S. Blanchard Jr.

Organizations

  • Langley Research Center

Tags

Communities of Interest

  • Weapons Technologies

DTIC Thesaurus Topics

  • Aerodynamic Characteristics
  • Angular Acceleration
  • Aspect Ratio
  • Base Pressure
  • Boundary Layer
  • Center Of Gravity
  • Drag
  • Dynamic Pressure
  • Equations
  • Equations Of Motion
  • Free Flight
  • Free Stream
  • Leading Edges
  • Mach Number
  • Rocket Models
  • Wind Tunnel Tests
  • Wind Tunnels

Technology Areas

  • Hypersonics