EXPANSIVE FLOW TABLES PERTINENT TO JET FLOW CALCULATIONS

Abstract

Charts and tables are presented for determining approximate values of the initial turning angles and the boundary shapes of jets exhausting to low ambient temperatures. The tables have been compiled to facilitate calculations pertaining to jet flow for various ratios of specific heats from 1.10 to 1.667 and Mach numbers from 1.0000 to 100.00. The ratios p/p sub t and A/A at the nozzle throat and the Prandtl-Meyer angle are given for each Mach number and ratio of specific heats.

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Document Details

Document Type
Technical Report
Publication Date
Apr 01, 1964
Accession Number
AD0435470

Entities

People

  • S. C. Lyons

Organizations

  • Arnold Engineering Development Complex

Tags

Communities of Interest

  • Air Platforms
  • Materials and Manufacturing Processes

DTIC Thesaurus Topics

  • Abstracts
  • Air Force
  • Boundaries
  • Flow
  • Government Procurement
  • Governments
  • Jet Flow
  • Mach Number
  • Nomenclature
  • Nozzles
  • Specific Heat
  • United States
  • United States Government
  • Wind Tunnels

Fields of Study

  • Physics

Readers

  • Aerodynamics/Aeronautics.
  • Business Analytics
  • Fluid Dynamics.