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Three-dimensional Supersonic Flutter Model Tests Near Mach Number 1.5. Part 3: Experimental and Theoretical Data for Wings with Control Surfaces
Author(s): Asher, Gifford W., Weatherhill, Warren H.Corporate Author(s): Massachusetts Institute of Technology
Laboratory: Aircraft Laboratory
Date of Publication: 1958-01
Report number: WADC TR 54-113 Part 3
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A Method For The Approximate Solution Of The Heat Equation
Author(s): Weiner, Jerome H.Corporate Author(s): Institute Of Flight Structures,Columbia University
Laboratory: Aircraft Laboratory
Date of Publication: 1955-03
Report number: WADC TR 54-427
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Thermal Stress Analysis For Aircraft Structures Part II. Bibliography
Author(s): Boley, Bruno A., Weiner, Jerome H.Corporate Author(s): Institute Of Flight Structures, Department Of Civil Engineering and Engineering Mechanics, Columbia University.
Laboratory: Aircraft Laboratory
Date of Publication: 1955-11
Report number: WADC TR 56-102 Part 2
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Structural Design For Aerodynamic Heating. Part I: Design Information
Author(s): Dukes, W. H., Schnitt, A.Corporate Author(s): Bell Aircraft Corpoartion
Laboratory: Aircraft Laboratory
Date of Publication: 1955-10
Report number: WADC TR 55-305 Part 1
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Aeroelastic Effects On Dynamic Longitudinal Stability
Author(s): Goland, Martin, Luke, Yudell L.Corporate Author(s): Midwest Research Inst Kansas City MO
Laboratory: Aircraft Laboratory
Date of Publication: 1953-07
Report number: WADC TR 53-29
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Effects of Spring and Inertia Devices on the Longitudinal Stability of Aircraft
Author(s): Goldberg, Joseph H.Corporate Author(s): Princeton University
Laboratory: Aircraft Laboratory
Date of Publication: 1953-07
Report number: WADC TR 53-350
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Flight Test Investigation to Determine the Effectiveness of a Rocket as an Emergency Spin Recovery Device: Phase II
Author(s): Farmer, G. H.Corporate Author(s): North American Aviation, Inc.
Laboratory: Aircraft Laboratory
Date of Publication: 1953-08
Report number: WADC TR 53-396
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Effects of Airplane Elasticity and Unsteady Flow on Longitudinal Stability
Author(s): Goland, Martin, Luke, Tudell L., Sacks, IrvingCorporate Author(s): Midwest Research Institute
Laboratory: Aircraft Laboratory
Date of Publication: 1953-11
Report number: WADC TR 53-425
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Subsonic Flutter Tests of an Unswept All-Movable Horizontal Tail
Author(s): Hoffman, Niles R., Spielberg, Irvin N.Corporate Author(s): Aircraft Laboratory
Laboratory: Aircraft Laboratory
Date of Publication: 1954-03
Report number: WADC TR 54-53
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Theoretical Studies of the Effects of Aspect Ratio on Flutter
Author(s): Goland, Martin, Luke, Y. L., Dengler, M. A.Corporate Author(s): Midwest Research Institute
Laboratory: Aircraft Laboratory
Date of Publication: 1954-06
Report number: WADC TR 54-29
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- Ambrosio, Alphonso (6)
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- Massachusetts Institute of Technology (13)
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