Aerodynamic Interference Effects Caused By Parallel Staged Simple Aerodynamic Configurations At Mach Numbers Of 3 And 6


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Aerodynamic Interference Effects Caused by Parallel-staged Simple Aerodynamic Configurations at Mach Numbers of 3 and 6


Aerodynamic Interference Effects Caused by Parallel-staged Simple Aerodynamic Configurations at Mach Numbers of 3 and 6

Author: John P. Decker

language: en

Publisher:

Release Date: 1969


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Aerodynamic characteristics effected by parallel- staged simple aerodynamic configurations at Mach numbers of 3 and 6.

NASA Technical Note


NASA Technical Note

Author:

language: en

Publisher:

Release Date: 1969


DOWNLOAD