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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