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Energy efficient engine low-pressure compressor component test hardware detailed design report

Author
Halle, J. E.
Published
Jun 1, 1981.
Physical Description
1 electronic document
Additional Creators
Michael, C. J.
Online Version

Availability

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Restrictions on Access
Unclassified, Unlimited, Publicly available.
Free-to-read Unrestricted online access
Summary
The aerodynamic and mechanical design description of the low pressure compressor component of the Energy Efficient Engine were used. The component was designed to meet the requirements of the Flight Propulsion System while maintaining a low cost approach in providing a low pressure compressor design for the Integrated Core/Low Spool test required in the Energy Efficient Engine Program. The resulting low pressure compressor component design meets or exceeds all design goals with the exception of surge margin. In addition, the expense of hardware fabrication for the Integrated Core/Low Spool test has been minimized through the use of existing minor part hardware.
Other Subject(s)
Collection
NASA Technical Reports Server (NTRS) Collection.
Note
Document ID: 19830022156.
Accession ID: 83N30427.
PWA-5594-157.
NAS 1.26:165354.
NASA-CR-165354.
Terms of Use and Reproduction
No Copyright.
View MARC record | catkey: 15711992