ROLLING MOMENT OF FLAT WINGS IN AN OBLIQUE SUPERSONIC GAS FLOW,

Abstract

The coefficient of the rolling moment is de termined for triangular, quadrangular, and pentagonal wings in an oblique supersonic gas flow. The problem is solved in a linearized set up by means of linear theory methods. (Author)

Document Details

Document Type
Technical Report
Publication Date
Jun 20, 1963
Accession Number
AD0413599

Entities

People

  • Yu.i. Krasilnikov

Organizations

  • National Air and Space Intelligence Center

Tags

DTIC Thesaurus Topics

  • Flow
  • Gas Flow

Fields of Study

  • Physics

Readers

  • Control Systems Engineering.
  • Fluid Dynamics.

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Boundary Layers
  • Hypersonics - Hypersonic Flight