Publication Date:
2019-07-13
Description:
The suitability of large engine technology to reduce noise, emissions, and fuel consumption of small turbine engines and develop new technology where required is determined. The design, fabrication, assembly, test, and delivery of the experimental engines to NASA are discussed.
Keywords:
AIRCRAFT PROPULSION AND POWER
Type:
NASA-TM-X-73564
,
E-9008
,
Intern. Gas Turbine Conf.; Mar 27, 1977 - Mar 31, 1977; Philadelphia, PA; United States
Format:
application/pdf
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