EXPERIMENTAL INVESTIGATION OF THE AERODYNAMIC CHARACTERISTICS OF AN AIR- TO-AIR MISSILE EMPLOYING CRUCIFORM WINGS AND TAIL OF RECTANGULAR PLAN FORM AT MACH NUMBERS OF 1.4 AND 1.9

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Document Details

Document Type
Technical Report
Publication Date
Feb 16, 1953
Accession Number
AD0001475

Entities

People

  • Merrill H. Mead

Organizations

  • National Aeronautics and Space Administration

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Aerodynamic Characteristics
  • Aeronautical Laboratories
  • Aircrafts
  • Aspect Ratio
  • Bodies
  • Cruciform Wings
  • Dynamic Pressure
  • Lifting Surfaces
  • Mach Number
  • Measurement
  • National Security
  • Reynolds Number
  • Security
  • Static Pressure
  • Supersonic Wind Tunnels
  • Wind Tunnel Tests
  • Wind Tunnels