Exhaust turbine and jet propulsion systems / by K. Leist and E. Knörnschild.
DVL experimental and analytical work on the cooling of turbine blades by using ram air as the working fluid over a sector or sectors of the turbine annulus area is summarized. The subsonic performance of ram-jet, turbo-jet, and turbine-propeller engines with both constant pressure and pulsating-flow...
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| Format: | Government Document Book |
| Language: | English |
| Published: |
Washington, D.C. :
National Advisory Commitee for Aeronautics,
[1951]
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| Series: | Technical memorandum (United States. National Advisory Committee for Aeronautics) ;
no. 1294. |
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| Summary: | DVL experimental and analytical work on the cooling of turbine blades by using ram air as the working fluid over a sector or sectors of the turbine annulus area is summarized. The subsonic performance of ram-jet, turbo-jet, and turbine-propeller engines with both constant pressure and pulsating-flow combustion is investigated. Comparison is made with the performance of a reciprocating engine and the advantages of the gas turbine and jet-propulsion engines are analyzed. Nacelle installation methods and power-level control are discussed. |
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| Item Description: | "April 1951." NACA TM Number 1294. Translated from Zentrale fur wissenschaftliches Berichtswesen bei der Deutschen Versuchsanstalt fur Luftfahrt E.V., Berlin-Adlershof. Forschungsbericht Number 1069, May 15, 1939, by the National Advisory Commitee for Aeronautics. |
| Physical Description: | 48 pages : illustrations ; 27 cm. |