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.

Limit your search

Publication Date

Laboratory

Report Availability

7 reports

Thermo-Elastic Stresses And Deflections In Beam-Columns

Author(s): Bruno A. Boley; Harold Mechanic
Corporate Author: Institute Of Air Flight Structures, Columbia University
Laboratory: Aircraft Laboratory
Date of Publication: 1954-03
Report Number: WADC TR 54-425
full text unavailable

Thermo-Elastic Stresses And Deflections In Thin-Walled Beams

Author(s): Bruno A. Boley; Irwin S. Tolins
Corporate Author: Institute Of Flight Structures, Columbia University
Laboratory: Aircraft Laboratory
Date of Publication: 1954-12
Report Number: WADC TR 54-426
full text unavailable

Method For Predicting Dynamic Landing Loads

Author(s): Richard L. Eisenman, Edward H. Kramer
Corporate Author: Aircraft Laboratory
Laboratory: Aircraft Laboratory
Date of Publication: 1954-09
Report Number: WADC TR 54-28
full text unavailable

Subsonic Flutter Tests of an Unswept All-Movable Horizontal Tail

Author(s): Niles R. Hoffman; Irvin N. Spielberg
Corporate Author: Aircraft Laboratory
Laboratory: Aircraft Laboratory
Date of Publication: 1954-03
Report Number: WADC TR 54-53
full text unavailable

Theoretical Studies of the Effects of Aspect Ratio on Flutter

Author(s): Martin Goland; Y. L. Luke; M. A. Dengler
Corporate Author: Midwest Research Institute
Laboratory: Aircraft Laboratory
Date of Publication: 1954-06
Report Number: WADC TR 54-29
full text unavailable

Subsonic Flutter Model Tests of Wings Carrying Heavy Tip Pods. Part 2. Swept Wings

Author(s): W. G. Brady; H. G. Maier; Walter T. Pargoff
Corporate Author: Cornell Aeronautical Laboratory, Inc.
Laboratory: Aircraft Laboratory
Date of Publication: 1954-11
Report Number: WADC TR 53-161 Part 2
full text unavailable

Flutter Characteristics of a T-Tail

Author(s): G. E. Pengelley, L. E. Wilson, T. B. Epperson, G. E. Ransleben
Corporate Author: Southwest Research Institute
Laboratory: Aircraft Laboratory
Date of Publication: 1954-11
Report Number: WADC TR 52-162
full text unavailable