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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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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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Subsonic Oscillatory or Steady Airloads on Wings with Control Surfaces and Other Discontinuities
Author(s): Ashley, Holt
Corporate Author(s): Stanford University, Department of Aeronautics and Astronautics
Laboratory: Air Force Office of Scientific Research
Date of Publication: 1967-12
Report number: AFOSR 68-0419

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