EFFECTS OF TWO SPINNER SHAPES ON THE PRESSURE RECOVERY IN AN NACA 1-SERIES D-TYPE COWL BEHIND A THREE-BLADE PROPELLER AT MACH NUMBERS UP TO 0.80

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Document Details

Document Type
Technical Report
Publication Date
Mar 19, 1954
Accession Number
AD0029126

Entities

People

  • Ashley J. Molk
  • Robert M. Reynolds

Organizations

  • National Aeronautics and Space Administration

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Aeronautical Laboratories
  • Air Flow
  • Blades
  • Boundaries
  • Boundary Layer
  • Coefficients
  • Diameters
  • Flow
  • Geometry
  • Government Procurement
  • Mach Number
  • Mass Flow
  • Propeller Blades
  • Propellers
  • Static Pressure
  • Turbines
  • Wind Tunnels