The goal of the Contrails project is to help preserve and disseminate the technical record of 20th century aerospace research, highlighting in particular the research endeavors of the Illinois Tech community.

1 report

An Investigation of Separated Flow About a Hemisphere-Cylinder at 0- to 19-Deg Incidence in the Mach Number Range from 0.6 to 1.5

Author(s): Hsieh, T.
Corporate Author: ARO, Inc.
Laboratory: Propulsion and Wind Tunnel Facility
Date of Publication: 1976-11
Report Number: AEDC TR 76-112
full text by request