Drag and Longitudinal Trim at Low Lift of the North American YF-100A Airplane at Mach Numbers from 0.76 to 1.77 as Determined from the Flight Test of a 0.11-Scale Rocket Model Page: 1 of 25
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YF-100A AIRPLANE AT MACH NUMBERS FROM 0.76 TO 1.77
RESEARCH FROM THE FLIGHT TEST OF ANU
U.By Willard S. Blanchar , Jr.
AS I ' FI M~lf T'E FLIGHT f TS T rF A
Langley Field, Va.
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ias 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
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Blanchard, Willard S., Jr. Drag and Longitudinal Trim at Low Lift of the North American YF-100A Airplane at Mach Numbers from 0.76 to 1.77 as Determined from the Flight Test of a 0.11-Scale Rocket Model, report, May 14, 1953; (digital.library.unt.edu/ark:/67531/metadc65341/m1/1/: accessed August 15, 2018), University of North Texas Libraries, Digital Library, digital.library.unt.edu; crediting UNT Libraries Government Documents Department.