A Sub-Scale Turbojet Test Cell for Design Evaluations and Analytical Model Validation

Abstract

A one-eighth scale (1/64 scale on mass flow) NARF Alameda turbojet test cell was designed and constructed. The test cell is to be employed for evaluation of optimum augmentor design and pollution abatement methods and for validation of analytical models. Initial evaluation of the test cell demonstrated its versatility and ease of operation as well as some deficiencies. Model operating characteristics and planned investigations are discussed.

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Document Details

Document Type
Technical Report
Publication Date
Sep 01, 1977
Accession Number
ADA049862

Entities

People

  • David W. Netzer
  • Holden W. Hewlett
  • P. J. Hickey

Organizations

  • Naval Postgraduate School

Tags

Communities of Interest

  • Air Platforms
  • Human Systems
  • Space

DTIC Thesaurus Topics

  • Acquisition
  • Afterburners
  • Air Ejectors
  • Air Supplies
  • Data Acquisition
  • Flow Visualization
  • Jet Aircraft
  • Jet Engine Fuels
  • Jet Engines
  • Measurement
  • Pressure Measurement
  • Ramjet Engines
  • Static Pressure
  • Test Facilities
  • Turbine Components
  • Turbines
  • Turbofan Engines

Readers

  • Combustion and Flow Dynamics.
  • Logistics and Supply Chain Management.
  • Software Engineering