Analysis of Turbine Stator Adjustment Required for Compressor Design-Point Operation in High Mach Number Supersonic Turbojet Engines (Listing Multiple Pages).
Filename | Size | Format | Download |
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19930087802.pdf | 1.6 MB | application/pdf | Download |
Filename | Size | Format | Download |
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19930087802.pdf | 1.6 MB | application/pdf | Download |