NASA NTRS · 19690000563
Experimental program to investigate transonic flow around protuberances
Abstract
Transient and steady state aerodynamic flow of turbulent boundary layers are investigated for generalized cylindrical projections and several specific configurations used on the Saturn 5 launch vehicle. A transonic wind tunnel gave generalized information.
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Robertson, J. E.. 1969-11-01. Experimental program to investigate transonic flow around protuberances. https://ntrs.nasa.gov/citations/19690000563
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