PRESSURE DISTRIBUTIONS AT MACH NUMBERS OF 1.6 AND 1.9 OF A CONICALLY CAMBERED WING OF TRIANGULAR PLAN FORM WITH AND WITHOUT PYLON-MOUNTED ENGINE NACELLES

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Document Details

Document Type
Technical Report
Publication Date
Apr 20, 1956
Accession Number
AD0092660

Entities

People

  • E. R. Phelps

Organizations

  • National Aeronautics and Space Administration

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Aeronautical Laboratories
  • Aircrafts
  • Aspect Ratio
  • Dynamic Pressure
  • Engine Nacelles
  • Flow
  • Leading Edges
  • Load Distribution
  • Mach Number
  • Measurement
  • Pressure Distribution
  • Pressure Gradients
  • Pressure Measurement
  • Shock Waves
  • Static Pressure
  • United States Government
  • Wind Tunnels