Aerodynamic Heating and Boundary-Layer Transition on a 1/10-Power Nose Shape in Free Flight at Mach Numbers Up to 6.7 and Free-Stream Reynolds Numbers Up To 16 x 10(Exp 6)

Author: Garland, Benjamine J.
Additional Authors: Swanson, Andrew G.
Year: 1957
Document Type: N/A
Series: NACA Research Memorandums
Report Number: NACA-RM-L57E14a
Link: https://digital.library.unt.edu/ark:/67531/metadc63557/

< New search