Effect of Blade-Section Camber on Aerodynamic Characteristics of Full-Scale Supersonic-Type Propellers at Mach Numbers to 1.04 Page: 1 of 81
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I RM L56E10RESEARCH MEMORANDUM
EFFECT OF BLADE-SECTION CAMBER ON AERODYNAMIC
CHARACTERISTICS OF FULL-SCALE SUPERSONIC -TYPE
PROPELLERS AT MACH NUMBERS TO 1.04
By Julian D. Maynard, John M. Swihart,
and Harry T. Norton, Jr.
Langley Aeronautical Laboratory
Langley Field, Va.
CLASSIFIED DOCUMENT
This material contains information affecting the National Defense of the United States within the meaning
of the espionage laws, Title 18, U.S.C., Secs. 793 and 794, the transmission or revelation of which in any
manner to an unauthorized person is prohibited by law.
NATIONAL ADVISORY COMMITTEE
FOR AERONAUTICS
WASHINGTON
October 19, 1956 e"j#r!:.- i/
NNW %Nor 5---"-W-mm---Nmrw
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Maynard, Julian D.; Swihart, John M. & Norton, Harry T., Jr. Effect of Blade-Section Camber on Aerodynamic Characteristics of Full-Scale Supersonic-Type Propellers at Mach Numbers to 1.04, report, October 19, 1956; (https://digital.library.unt.edu/ark:/67531/metadc62729/m1/1/: accessed April 18, 2024), University of North Texas Libraries, UNT Digital Library, https://digital.library.unt.edu; crediting UNT Libraries Government Documents Department.