INTERNAL PERFORMANCE CHARACTERISTICS OF SHORT CONVERGENT-DIVERGENT EXHAUST NOZZLES DESIGNED BY THE METHOD OF CHARACTERISTICS

Abstract

An evaluation of the internal performance characteristics of short nozzles designed by the method of characteristics was obtained over a range of nozzle pressure ratios from 1.5 to 22.

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Document Details

Document Type
Technical Report
Publication Date
Jul 24, 1956
Accession Number
AD0102311

Entities

People

  • H. G. Krull
  • William T. Beale

Organizations

  • National Aeronautics and Space Administration

Tags

DTIC Thesaurus Topics

  • Air
  • Air Flow
  • Air Pressure
  • Coefficients
  • Conical Nozzles
  • Exhaust Nozzles
  • Flow
  • Government Procurement
  • Governments
  • Labyrinth Seals
  • Method Of Characteristics
  • Nozzles
  • Pressure Measurement
  • Sea Level
  • Static Pressure
  • United States
  • United States Government

Readers

  • Combustion and Flow Dynamics.