Component and over-all performance evaluation of an axial-flow turbojet engine over a range of engine-inlet Reynolds numbers Page: 1 of 44
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A cSlJ N~ RrJ"tIa IVIAT ION 2
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COMPONENT AND OVER-ALL PERFORMANCE EVALUATION
OF AN AXIAL-FLOW TURBOJET ENGINE OVER A RANGE
j OF ENGINE-INLET REYNOLDS NUMBERS
By Curtis L. Walker, S. C. Huntley
and W. M. Braithwaite
Lewis Flight Propulsion Laboratory
CLASSIFICATION d oxio
By authority of ,......... Date
4rn/3-n' 7 ..r.~Cc& -rftt n ......
This material conta ins I nftr on affecting the l onal Deane of the united States within the m ann
of the espionage laws, Title 18, US.C., Scos. 795 aol 794, the transmit on or revelation of which In icy
manner to an tnuthorised person is probtited by law.
NATIONAL ADVISORY COMMITTEE
2 July 10, 1952
6Nf DENIAL N .. .....
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Walker, Curtis L.; Huntley, S. C. & Braithwaite, W. M. Component and over-all performance evaluation of an axial-flow turbojet engine over a range of engine-inlet Reynolds numbers, report, July 10, 1952; (https://digital.library.unt.edu/ark:/67531/metadc59177/m1/1/: accessed April 22, 2019), University of North Texas Libraries, Digital Library, https://digital.library.unt.edu; crediting UNT Libraries Government Documents Department.