Hostname: page-component-848d4c4894-ttngx Total loading time: 0 Render date: 2024-06-01T23:00:27.648Z Has data issue: false hasContentIssue false
  • English
  • Français

The Design and Development of a Large Supersonic Free-Jet Test Cell

Published online by Cambridge University Press:  04 July 2016

P. F. Ashwood
P. F. Ashwood*
Affiliation:
NGTE, Pyestock
Get access Rights & Permissions [Opens in a new window]

Extract

The NGTE Engine Test Facility has five test cells in current use and between them they can test aircraft powerplants over a wide range of operation at the precise conditions encountered in flight. Two basic testing techniques are employed—“connected testing”, in which air is piped directly to the engine compressor at the pressure and temperature conditions provided in flight by the intake, and “free-jet testing”.

Type
Symposium on Altitude Testing
Information
The Aeronautical Journal , Volume 74 , Issue 711 , March 1970 , pp. 205 - 212
Copyright
Copyright © Royal Aeronautical Society 1970 

Access options

Get access to the full version of this content by using one of the access options below. (Log in options will check for institutional or personal access. Content may require purchase if you do not have access.)

References

1. Mcgarry, J. B. The development of a variable Mach number effuser. ARC R & M 3097.Google Scholar