SUPERSONIC WAVE DRAG OF NONLIFTING DELTA WINGS WITH LINEARLY VARYING THICKNESS RATIO

Open PDF

Document Details

Document Type
Technical Report
Publication Date
Dec 01, 1952
Accession Number
AD0001445

Entities

People

  • Arthur Henderson Jr.

Organizations

  • Langley Research Center

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Aeronautical Laboratories
  • Boundaries
  • Cartesian Coordinates
  • Delta Wings
  • Differential Equations
  • Distribution Functions
  • Drag Reduction
  • Dynamic Pressure
  • Equations
  • Free Stream
  • Leading Edges
  • Mach Number
  • Partial Differential Equations
  • Pressure Distribution
  • Static Pressure
  • Trailing Edges
  • Two Dimensional

Technology Areas

  • Hypersonics