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Historical

SAE AIR5295

Design Considerations for Enclosed Turboprop Engine Test Cells

Standard by SAE International, 2007-11-15

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  • Language: English
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About This Item

This document is offered to provide state-of-the-art information about design factors that must be considered in the design of new or significantly modified engine test cells used to test propeller equipped turboprop engines in either QEC or bare engine configurations. The report does not address design considerations for test cells designed to test turboprop engines with dynamometer type load absorption devices because they are essentially tested as turboshaft engines. Design considerations for those test cells are presented in AIR4989, Reference 2.1.
SKU: 04176423c972

  • Publication Date: 2007-11-15
  • Standard Status: historical
  • Publisher: SAE International
  • Document Type: Aerospace Standard
  • Subject: Test facilities, Exhaust gas recirculation (EGR), Nitrogen oxides, Turboprop engines, Performance tests, Engine mounts, Jet engines, Carbon dioxide, Cost analysis
  • Official SAE: Doi link
  • New Version Available: AIR5295B (2025-11-19)
  • Previous Version: AIR5295A (2018-11-21)
  • This Version: AIR5295 (2007-11-15)

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