CALCULATIONS OF EQUILIBRIUM GAS FLOWS IN SUPERSONIC NOZZLES (RASCHET RAVNOVESNYKH TECHENII GAZA V SVERKHZVUKOVYKH SOPLAKH),

Abstract

The book is intended for technical personnel concerned with design and operation of nozzles. The procedure and formulas for calculating of gas flow parameters in plane and axisymmetric nozzles are presented. Steady equilibrium flows of an imperfect gas with arbitrary thermodynamic characteristics are examined. Equations are given for a particular case of an adiabatic flow of a perfect gas. Gas flows in nozzles with plane nozzles and with a break in the generatrix at the discharge section, as well as in annular nozzles are examined. The method of characteristics properly adapted for the computation on electronic computers is utilized. (Author)

Document Details

Document Type
Technical Report
Publication Date
Jan 10, 1968
Accession Number
AD0675564

Entities

People

  • O. N. Katskova

Organizations

  • National Air and Space Intelligence Center

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Annular Nozzles
  • Axisymmetric
  • Computations
  • Computers
  • Equations
  • Flow
  • Gas Flow
  • Mathematics
  • Method Of Characteristics
  • Nozzles
  • Supersonic Nozzles

Fields of Study

  • Physics

Readers

  • Calculus or Mathematical Analysis
  • Combustion and Flow Dynamics.
  • Information Retrieval

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Flight
  • Hypersonics - Hypersonic Flow
  • Microelectronics
  • Microelectronics - Microelectromechanical Systems