Cruise performance of an isolated 1.15 pressure ratio turbofan propulsion system simulator at Mach numbers from 0.6 to 0.85 /
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| Format: | Book |
| Language: | English |
| Published: |
Washington, D.C. : [Springfield, Va. :
National Aeronautics and Space Administration ; For sale by the National Technical Information Service],
1974
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| Series: | NASA technical memorandum ;
3064 |
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| Call Number: |
NASA TM X3064 |
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