Aerodynamic-Derivative Characteristics of the X-15 Research Airplane as Determined from Flight Tests for Mach Numbers from 0.6 to 3.4

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Document Details

Document Type
Technical Report
Publication Date
Jan 01, 1962
Accession Number
AD0270812

Entities

People

  • Glenn H. Robinson
  • Herman A. Rediess
  • Roxanah B. Yancey

Organizations

  • National Aeronautics and Space Administration

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Accuracy
  • Aircrafts
  • Airframes
  • Airplanes
  • Control Surfaces
  • Engines
  • Flight Simulators
  • Horizontal Stabilizers
  • Low Angles
  • Mach Number
  • Research Aircraft
  • Resonant Frequency
  • Rocket Engines
  • Simulators
  • Surfaces
  • Swept Wings
  • Wind Tunnels