PRESSURE RECOVERY AND DRAG CHARACTERISTICS OF A FORWARD LOCATED CIRCULAR SCOOP INLET AS DETERMINED FROM FLIGHT TESTS FOR MACH NUMBERS FROM 0.8 TO 1.6

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Document Details

Document Type
Technical Report
Publication Date
Apr 08, 1954
Accession Number
AD0029315

Entities

People

  • Charles F. Merlet

Organizations

  • Langley Research Center

Tags

Communities of Interest

  • Weapons Technologies

DTIC Thesaurus Topics

  • Accuracy
  • Aeronautical Laboratories
  • Aircrafts
  • Diameters
  • Flight
  • Flow
  • Flow Rate
  • Free Flight
  • Free Stream
  • Mach Number
  • Mass Flow
  • Measurement
  • Parabolic Bodies
  • Pressure Distribution
  • Pressure Measurement
  • Reynolds Number
  • Static Pressure