DETERMINATION OF THE PROFILE OF LEAST RESISTANCE OF AN ANNULAR WING

Abstract

A thin axisymmetric wing in a supersonic flow is studied to determine the profile of least resistance of an annular wing.

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Document Details

Document Type
Technical Report
Publication Date
Jun 11, 1963
Accession Number
AD0410936

Entities

People

  • B. I. Borisov

Organizations

  • National Air and Space Intelligence Center

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Air Force
  • Air Force Facilities
  • Boundaries
  • Department Of Defense
  • Equations
  • Foreign Technology
  • Government Procurement
  • Governments
  • Integrals
  • Method Of Characteristics
  • Resistance
  • Ring Wings
  • Supersonic Flow
  • Translations

Fields of Study

  • Physics

Technology Areas

  • Hypersonics