ROCKET-MODEL INVESTIGATION OF THE LONGITUDINAL STABILITY, DRAG, AND DUCT PERFORMANCE OF A 60 DEGREE DELTA-WING CANARD AIRCRAFT WITH TWIN SIDE INLETS AT MACH NUMBERS FROM 0.80 TO 1.70

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Document Details

Document Type
Technical Report
Publication Date
Mar 01, 1954
Accession Number
AD0029316

Entities

People

  • Aleck C. Bond
  • Andrew G. Swanson

Organizations

  • Langley Research Center

Tags

Communities of Interest

  • Weapons Technologies

DTIC Thesaurus Topics

  • Accuracy
  • Aeronautical Laboratories
  • Aircrafts
  • Base Pressure
  • Boundary Layer
  • Center Of Gravity
  • Control Surfaces
  • Control Systems
  • Free Stream
  • Mach Number
  • Mass Flow
  • Measurement
  • Measuring Instruments
  • Pressure Measurement
  • Static Pressure
  • Telemetry
  • Wind Tunnels