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Flutter Characteristics Of Low Aspect Ratio wings In Incompressible Flow. Part I: Development Of The Basic Theory Of The Method
Author(s): Lawrence, H. R., Stone, H. N.Corporate Author(s): Cornell Aeronautical Laboratory, Inc.
Laboratory: Aircraft Laboratory
Date of Publication: 1957-05
Report number: WADC TR 54-412 Part 1
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Development Of Equipment For The Experimental Measurement Of The Moments Of Inertia, And Product Of Inertia Of Aircraft
Author(s): Woodward, Claude R.Corporate Author(s): Cornell Aeronautical Laboratory, Inc.
Laboratory: Aircraft Laboratory
Date of Publication: 1954-06
Report number: WADC TR 54-237
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Flutter Tests of Large Straight Wing Models at High Subsonic Speeds
Author(s): White, Richard P., Jr.Corporate Author(s): Cornell Aeronautical Laboratory, Inc.
Laboratory: Aircraft Laboratory
Date of Publication: 1955-12
Report number: WADC TR 55-334
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