Certain Modifications of Gasodynamical Total Impulse Functions,

Abstract

In the study it is shown how the gasodynamical functions are modified if they are used for calculating the total impulse flow of a plane boundary layer given an arbitrary orientation of the reference surface. Moreover, gasodynamical functions are derived for two-layer flows consisting of a boundary layer and a homogeneous layer of some thickness taken in a streamline flow or at the nucleus.

Document Details

Document Type
Technical Report
Publication Date
Nov 26, 1974
Accession Number
ADA004348

Entities

People

  • B. S. Vinogradov

Organizations

  • National Air and Space Intelligence Center

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Boundaries
  • Boundary Layer
  • Geometry
  • Layers
  • Orientation (Direction)
  • Thickness

Fields of Study

  • Physics

Readers

  • Control Systems Engineering.
  • Fluid Dynamics.