RESULTS OF CALCULATION OF THE BOUNDARY LAYER OF BLUNTED CONES IN SUPERSONIC FLOW.

Abstract

The paper presents the results of the calculation of the boundary layer of spherically blunted cones in supersonic airflow for a given (constant) wall temperature and for a thermally insulated wall.

Document Details

Document Type
Technical Report
Publication Date
Mar 01, 1966
Accession Number
AD0631971

Entities

People

  • A. L. Ankudinov

Organizations

  • American Meteorological Society

Tags

DTIC Thesaurus Topics

  • Boundaries
  • Boundary Layer
  • Layers
  • Supersonic Flow

Fields of Study

  • Physics

Readers

  • Fluid Dynamics.

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Boundary Layers
  • Hypersonics - Hypersonic Flow
  • Microelectronics
  • Microelectronics - Graphene