EFFECT OF LEADING-EDGE DROOP ON THE AERODYNAMIC AND LOADING CHARACTERISTICS OF A 4-PERCENT-THICK UNSWEPT-WING-FUSELAGE COMBINATION AT TRANSONIC SPEEDS

Open PDF

Document Details

Document Type
Technical Report
Publication Date
May 23, 1956
Accession Number
AD0094328

Entities

People

  • James W. Schmeer

Organizations

  • National Aeronautics and Space Administration

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Aerodynamic Characteristics
  • Aerodynamic Configurations
  • Airfoils
  • Aspect Ratio
  • Bending Moments
  • Geometry
  • Governments
  • Leading Edge Flaps
  • Leading Edges
  • Mach Number
  • Measurement
  • Pressure Distribution
  • Pressure Measurement
  • Reynolds Number
  • Shock Waves
  • Static Pressure
  • Two Dimensional