Experimental and Analytical Methods for the Determination of Connected- Pipe Ramjet and Ducted Rocket Inte rnal Performance (Methodes Experimentes et Analytiques pour la Determination en Conduite forcee des Performances des Statoreacteurs et des Statofusees)

Abstract

Connected-pipe, subsonic combustion ramjet and ducted rocket performance determination procedures used by the NATO countries have been reviewed and evaluated. A working document has been produced which provides recommended methods for reporting test results and delineates the parameters that are required to be measured. Explanations and detailed numerical examples are presented covering the determination of both theoretical and experimental performances, the use of air heaters and uncertainty and error analyses.

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Document Details

Document Type
Technical Report
Publication Date
Jul 01, 1994
Accession Number
ADA286624

Entities

Organizations

  • AGARD

Tags

Communities of Interest

  • Air Platforms
  • Weapons Technologies

DTIC Thesaurus Topics

  • Accuracy
  • Burning Rate
  • Combustion
  • Combustion Products
  • Computational Fluid Dynamics
  • Computational Science
  • Computer Programs
  • Heat Of Formation
  • Heat Transfer
  • Materials Processing
  • Materials Science
  • Materials Testing
  • Measurement
  • Measuring Instruments
  • Pressure Measurement
  • Rocket Engines
  • Test Facilities

Readers

  • Combustion and Flow Dynamics.
  • Small Business Innovation Research Program (SBIR) EDI Research and Innovation.
  • Systems Analysis and Design