NEWS OF THE INSTITUTES OF HIGHER LEARNING: AERONAUTICAL ENGINEERING (SELECTED ARTICLES)

Abstract

Contents: Investigation of the Working Cascades of Turbines at Supersonic Velocities, An Approximation Method for Calculating Steady State Uniform Gas Flow in a Tube with Equilibrium dissociation and Ionization, Taking into Account Resistance.

Open PDF

Document Details

Document Type
Technical Report
Publication Date
Mar 19, 1963
Accession Number
AD0402471

Entities

People

  • A. V. Gubarev
  • I. I. Suksov

Organizations

  • National Air and Space Intelligence Center

Tags

Communities of Interest

  • Energy and Power Technologies

DTIC Thesaurus Topics

  • Boundary Layer
  • Engineering
  • Equations
  • Flow
  • Flow Fields
  • Gas Flow
  • Heat Energy
  • Heat Transfer
  • Heat Transfer Coefficients
  • Heat Transmission
  • High Temperature
  • Leading Edges
  • Mach Number
  • Pressure Distribution
  • Radiation
  • Supersonic Flow
  • Thermodynamics

Fields of Study

  • Physics

Readers

  • Aerodynamics.
  • Library and Information Science/ Studies, Southeast Asia Studies, Bibliography of Vietnam and Lao Studies.
  • Molecular Photonics/Laser Physics

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Flight