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 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