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Three-dimensional Supersonic Flutter Model Tests Near Mach Number 1.5. Part 1: Model Design And Testing Techniques
Author(s): McCarthy, John F., Jr., Prigge, John S., Jr., Levy, Gilbert M., Asher, Gifford W.
Corporate Author(s): Aeroelastic And Structures Research Laboratory, Massachusetts Institute of Technology
Laboratory: Aircraft Laboratory
Date of Publication: 1955-12
Report number: WADC TR 54-113 Part 1
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The Effects Of Structural Elasticity On Aircraft Control Systems
Author(s): Howard, Vincent W.
Corporate Author(s): Aeroelastic And Structures Research Laboratory, Massachusetts Institute of Technology
Laboratory: Flight Control Laboratory
Date of Publication: 1956-06
Report number: WADC TR 56-166
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Investigation Of Rotor Response To Vibratory Aerodynamic Inputs. Part 1 Experimental Results And Correlation with Theory
Author(s): Ham, D., Moser, Herbert H., Zvara, John
Corporate Author(s): Aeroelastic And Structures Research Laboratory, Massachusetts Institute of Technology
Date of Publication: 1958-10
Report number: WADC TR 58-87 Part 1
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Investigation Of Rotor Response To Vibratory Aerodynamic Inputs. Part 2. An Aerodynamic Strip Theory For Rotary wings Executing Simple Harmonic Motions Near A Ground Plane
Author(s): Brunelle, J., Jr.
Corporate Author(s): Aeroelastic And Structures Research Laboratory, Massachusetts Institute of Technology
Date of Publication: 1958-10
Report number: WADC TR 58-87 Part 2
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Investigation Of Rotor Response To Vibratory Aerodynamic Inputs. Part 3. Threedimensional Effects On Unsteady Flow Through A Helicopter Rotor
Author(s): Ashley, Holt, Moser, Herbert H., Dugundji, John
Corporate Author(s): Aeroelastic And Structures Research Laboratory, Massachusetts Institute of Technology
Date of Publication: 1958-10
Report number: WADC TR 58-87 Part 3
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Development Of A Minature Pressure Transducer For Application To Airfoil Studies In The Shock Tube
Author(s): Ruetenik, J. Ray
Corporate Author(s): Aeroelastic And Structures Research Laboratory, Massachusetts Institute of Technology
Date of Publication: 1958-12
Report number: WADC TR 58-629
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Procedures For Including Temperature Effects In Structural Analysis Of Elastic wings. Part I: An Equivalent Plate Method Of Structural Analysis For Elevated Temperature Structures
Author(s): Mills, William R.
Corporate Author(s): Aeroelastic And Structures Research Laboratory, Massachusetts Institute of Technology
Date of Publication: 1958-01
Report number: WADC TR 57-754 Part 1
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Supersonic Flutter Trends As Revealed By Piston Theory Calculations
Author(s): Ashley, Holt, Zartarian, Garabed
Corporate Author(s): Aeroelastic And Structures Research Laboratory, Massachusetts Institute of Technology
Laboratory: Aircraft Laboratory
Date of Publication: 1958-05
Report number: WADC TR 58-74
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Gust Loading Of Rigid And Flexible Aircraft In Continous Atmospheric Turbulence
Author(s): Foss, Kenneth A., McCabe, Warren L.
Corporate Author(s): Aeroelastic And Structures Research Laboratory, Massachusetts Institute of Technology
Laboratory: Aircraft Laboratory
Date of Publication: 1958-01
Report number: WADC TR 57-704
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Transient And Nonlinear Effects On High Speed, Vibratory, Thermoelastic Instability Phenomena. Part II Aerothermoelastic Applications
Author(s): Brunelle, Eugene J., Jr.
Corporate Author(s): Aeroelastic And Structures Research Laboratory, Massachusetts Institute of Technology
Laboratory: Flight Dynamics Laboratory
Date of Publication: 1960-12
Report number: WADD TR 60-484 Part II

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