High-Speed Tests of Radial-Engine Nacelles on a Thick Low-Drag Wing

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Document Details

Document Type
Technical Report
Publication Date
May 01, 1942
Accession Number
ADA800964

Entities

People

  • John V. Becker

Organizations

  • Langley Research Center

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Aeronautical Laboratories
  • Aircrafts
  • Boundary Layer
  • Cooling
  • Drag
  • Dynamic Pressure
  • Engine Nacelles
  • Flow
  • Layers
  • Low Drag
  • Mach Number
  • Pressure Distribution
  • Pressure Gradients
  • Pressure Measurement
  • Propellers
  • Static Pressure
  • Wind Tunnels