Acceleration Characteristics of a Turbojet Engine With Variable-Position Inlet Guide Vanes Page: 1 of 31
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UNCLASSIIE-. .
Copy 6
-ACA
RESEARCH MEMORANDUM
ACCELERATION CHARACTERISTICS OF A TURBOJET ENGINE
WITH VARIABLE -POSITION INLET GUIDE VANES
By W. F. Dobson and Lewis E. Wallner
Lewis Flight Propulsion Laboratory
Cleveland, Ohio
CLASSIFICATION CHANGED IRAnRY COPY
To U.CL------UNCASSELED _ JJL ; 1955
AN lEY AEfROAUTTICA LABORATORY
of the esplaoage laws, Ti is, U.S.C.1 Secr. 793 and f94, the tranumisa ot or relation of Which in any
mannr to an nauuthorized person is prohibited by law.
NATIONAL ADVISORY COMMITTEE
FOR AERONAUTICS
r WASHINGTON
July 7, 1955
_,- ,UNCLASSIFIED
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Dobson, W. F. & Wallner, Lewis E. Acceleration Characteristics of a Turbojet Engine With Variable-Position Inlet Guide Vanes, report, July 7, 1955; (https://digital.library.unt.edu/ark:/67531/metadc60813/m1/1/: accessed April 19, 2024), University of North Texas Libraries, UNT Digital Library, https://digital.library.unt.edu; crediting UNT Libraries Government Documents Department.