Drag of a Wing-Body Configuration Consisting of a Swept-Forward Tapered Wing Mounted on a Body of Fineness Ratio 12 Measured During Free Fall at Transonic Speeds

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Document Details

Document Type
Technical Report
Publication Date
Mar 13, 1947
Accession Number
ADA800828

Entities

People

  • Charles W. Mathews
  • Jim R. Thompson

Organizations

  • Langley Research Center

Tags

DTIC Thesaurus Topics

  • Aeronautical Laboratories
  • Altitude
  • Barometric Pressure
  • Bodies
  • Coefficients
  • Fineness Ratio
  • High Altitude
  • Low Altitude
  • Mach Number
  • Measurement
  • Pressure Measurement
  • Sweptforward Wings
  • Wing Body Configurations