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

Shock-Tube Flow Investigations. Part 1. An Exploratory Study Of The Generation Of Blast -Type Profiles In The Shock Tube By The Reflection Method

Author(s): Lee, Robert C. K.
Corporate Author: Massachusetts Institute Of Technology
Laboratory: Aircraft Laboratory
Date of Publication: 1956-08
Report Number: WADC TR 54-383 Part 1
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