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Conceptual design studies of lift/cruise fans for military transportsA study program for conceptual design studies of remote lift and lift/cruise fan systems to meet the requirements of military V/STOL aircraft was conducted. Parametric performance and design data are presented for fans covering a range of pressure ratios, including both single and two stage fan concepts. The gas generator selected for these fan systems was the J101-GE-100 engine. Noise generation and transient response were determined for selected fan systems.
Document ID
19740022126
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Date Acquired
September 3, 2013
Publication Date
August 6, 1974
Subject Category
Propulsion Systems
Report/Patent Number
R74AEG283
NASA-CR-134636
Report Number: R74AEG283
Report Number: NASA-CR-134636
Accession Number
74N30239
Funding Number(s)
CONTRACT_GRANT: NAS3-17850
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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