THE EFFECT OF AN AXIALLY SYMMETRIC FUSELAGE ON THE NONSTATIONARY SUPERSONIC AIRLOADS ACTING ON A WING WITH SUPERSONIC EDGES

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Document Details

Document Type
Technical Report
Publication Date
May 01, 1954
Accession Number
AD0037709

Entities

People

  • Melvin Epstein

Tags

Communities of Interest

  • Air Platforms
  • Weapons Technologies

DTIC Thesaurus Topics

  • Aerodynamic Configurations
  • Aerodynamic Forces
  • Air Force
  • Aircrafts
  • Aspect Ratio
  • Coordinate Systems
  • Corporations
  • Engineering
  • Flow
  • Free Stream
  • Government Procurement
  • Governments
  • Grids
  • Leading Edges
  • Lifting Surfaces
  • Phase Shift
  • Translations

Technology Areas

  • Hypersonics