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![WADCTR55-318.pdf application/pdf thumbnail](https://digital2.library.iit.edu/files//medium/92c3e243c821ca7d07653724c5e5cc09fb8f7867.jpg)
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Effect Of Boundary Layer Profile, Air Speed, And System Geometry On The Stability Of Flow In Suction Systems
Author(s): Treanor, C. E., Flax, A. H.Corporate Author(s): Cornell Aeronautical Laboratory, Inc.
Laboratory: Aeronautical Research Laboratory
Date of Publication: 1956-07
Report number: WADC TR 55-318
![WADCTR55-156part02.pdf application/pdf thumbnail](https://digital2.library.iit.edu/files//medium/f25aab45789a0bee9228ebc7b984e1119bdff663.jpg)
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Installation of an Automatic Control System in a T-33 Airplane for Variable Stability Flight Research. Part 2. Detail Design, Fabrication and Installation
Author(s): Flight Research DepartmentCorporate Author(s): Cornell Aeronautical Laboratory, Inc.
Laboratory: Aeronautical Research Laboratory
Date of Publication: 1956-12
Report number: WADC TR 55-156 Part 2
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