Performance and load-range characteristics of turbojet engine in transonic speed range / Bernard Lubarsky.
An analysis was made of performance and load-range characteristics of turbojet engine for transonic speed range, altitudes from 10,000 to 70,000 feet, compressor pressure ratios from 2 to 30, and turbine-inlet temperature of 1700, 2000, and 2300 degrees R. Values of lift-drag and structure-to-gross-...
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| Format: | Government Document Book |
| Language: | English |
| Published: |
Washington, D.C. :
National Advisory Committee for Aeronautics,
1950.
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| Series: | Technical note (United States. National Advisory Committee for Aeronautics) ;
2088. |
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PASCAL Offsite
| Call Number: |
Y 3.N 21/5:6/2088
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| Y 3.N 21/5:6/2088 | Available Place a Hold |