APPROXIMATE COMPUTATION OF UNDEREXPANDED JET STRUCTURE.

Abstract

An investigation of the structure of a jet which exhausts at a pressure very much greater than the ambient pressure is carried out by an approximate analysis. This analysis has application in the description of the structure of a rocket exhaust at ionospheric altitudes, and of laboratory jet facilities of extreme pressure ratio.

Document Details

Document Type
Technical Report
Publication Date
Feb 01, 1965
Accession Number
AD0619777

Entities

People

  • F. A. Albini

Organizations

  • Institute for Defense Analyses

Tags

DTIC Thesaurus Topics

  • Altitude
  • Buildings And Structures
  • Computations
  • Mathematical Analysis
  • Mathematics
  • Observatories
  • Research Facilities
  • Rocket Exhaust
  • Test Facilities

Fields of Study

  • Physics

Readers

  • Combustion and Flow Dynamics.