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

Subsonic Oscillatory or Steady Airloads on Wings with Control Surfaces and Other Discontinuities

Author(s): Ashley, Holt
Corporate Author: Stanford University, Department of Aeronautics and Astronautics
Laboratory: Air Force Office of Scientific Research
Date of Publication: 1967-12
Report Number: AFOSR 68-0419
full text by request