The Origin and Distribution of Supersonic Store Interference From Measurement of Individual Forces on Several Wing-Fuselage-Store Configurations 5: Swept-Wing Heavy-Bomber Configuration With Large Store (Nacelle). Mach Number 2.01

Author: Carson, Harry W.
Year: 1956
Document Type: N/A
Series: NACA Research Memorandums
Report Number: NACA-RM-L55K15
Link: https://digital.library.unt.edu/ark:/67531/metadc61845/

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