NOZZLE DESIGN,

Abstract

Partial solutions to the approximation equations are given of the plane and axisymmetrical flow of a gas. It is possible to make use of these particular solutions in making the computations for designing nearsonic parts of nozzles. (Author)

Document Details

Document Type
Technical Report
Publication Date
Jul 14, 1966
Accession Number
AD0643632

Entities

People

  • I. M. Yurev

Organizations

  • National Air and Space Intelligence Center

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Computations
  • Equations
  • Mathematics

Fields of Study

  • Physics