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Three-Dimensional Supersonic Flutter Model Tests Near Mach Number 1.5. Part II. Experimental And Theoretical Data For Bare wings And wings with Tip Tanks
Author(s): McCarthy, John F., Jr., Martuccelli, John R., Asher, Gifford W., Zartarian, Garabed
Corporate Author(s): Massachusetts Institute of Technology
Laboratory: Aircraft Laboratory
Date of Publication: 1955-12
Report number: WADC TR 54-113 Part 2
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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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Unsteady Airloads On Pointed Airfoils And Slender Bodies At High Mach Numbers
Author(s): Zartarian, Garabed
Corporate Author(s): Aeroelastic And Structures Research Laboratory, Massachusetts Institute of Technology
Laboratory: Aircraft Laboratory
Date of Publication: 1959-12
Report number: WADC TR 59-583
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Theoretical And Experimental Studies On Airloads Related To Hypersonic Aeroelastic Problems Of General Slender Pointed Configurations
Author(s): Zartarian, Garabed, Tan Hsu, Pao
Corporate Author(s): Massachusetts Institute of Technology
Laboratory: Flight Dynamics Laboratory
Date of Publication: 1961-04
Report number: ASD TR 61-7
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Investigation On The Use Of Ascillatory Supersonic Aerodynamic Influence Coefficients
Author(s): Zartarian, Garabed
Report number: WADC TR 56-97 Part 1
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Rules For Application Of Oscillatory Supersonic Aerodynamic Influence Coefficinets
Author(s): Zartarian, Garabed
Report number: WADC TR 56-97 Part 2

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