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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
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Installation of an Automatic Control System in a T-33 Airplane for Variable Stability Flight Research. Part 1. - Preliminary Investigation and Design Studies
Author(s): Ball, J. N. (editor)Corporate Author(s): Flight Research Department, Cornell Aeronautical Laboratory, Inc.
Laboratory: Aeronautical Research Laboratory
Date of Publication: 1956-07
Report number: WADC TR 55-156 Part 1
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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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Experimental Investigation Of A Method Of Interference Drag Reduction Of A Swept Wing Aircraft By Means Of Fuselage Indentation
Author(s): Degen, M.Corporate Author(s): Brown Univ Providence RI
Laboratory: Aeronautical Research Laboratory
Date of Publication: 1956-03
Report number: WADC TR 55-12
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Dynamic System Studies: Aerodynamic Studies
Author(s): Saarlas, M., Krzywoblocki, M.Z.Corporate Author(s): University Of Chicago, University of Illinois
Laboratory: Aeronautical Research Laboratory
Date of Publication: 1956-09
Report number: WADC TR 54-250 Part 16
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An Elementary Approach To The Analysis Of Variance
Author(s): Rider, Paul ReeceCorporate Author(s): Aeronautical Research Laboratory
Laboratory: Aeronautical Research Laboratory
Date of Publication: 1956-02
Report number: WADC TR 56-20
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Flight Evaluations of the Effect of Variable Phugoid Damping in a JTB-26B Airplane
Author(s): Newell, Fred, Rhoads, Donald W.Corporate Author(s): Cornell Aeronautical Laboratory
Laboratory: Aeronautical Research Laboratory
Date of Publication: 1956-12
Report number: WADC TR 56-223
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