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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
Author:
Blanchard, Willard S., Jr.
Year:
1953
Document Type:
N/A
Series:
NACA Research Memorandums
Report Number:
NACA-RM-SL53E11a
Link:
https://digital.library.unt.edu/ark:/67531/metadc65341/
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