Contrails
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.

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2 reports

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): T. Hsieh
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

An Aerodynamic Coefficient Prediction Technique for Slender Bodies with Low Aspect Ratio Fins at Mach Numbers from 0.6 to 3.0 and Angles of Attack from 0 to 180 Degrees

Author(s): William B. Baker, Jr.
Corporate Author: ARO, Inc.
Laboratory: Propulsion and Wind Tunnel Facility
Date of Publication: 1978-03
Report Number: AEDC TR 77-97
full text by request