Scholarly Works - Reports
Report
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December 1, 1987
Recent interest in supersonic and hypersonic flight has renewed interest in developing propulsion systems which include a supersonic axial flow compressor. An important design consideration for the blades in such a compressor is aeroelastic stability. This ...
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Report
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June 1, 1986
This paper uses a typical section model to analytically investigate the effect of mass balancing as applied to hollow, supersonic fan blades. A procedure to determine the best configuration of an internal balancing mass to provide flutter alleviation is de ...
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Report
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September 1, 1985
This publication gives the complete theoretical and experimental results of the first phase of a joint government/industry/university research study on the vibration characteristics of twisted cantilever plates. The study was conducted to generate an exper ...
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Report
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March 1, 1985
This paper presents a structural and aeroelastic analysis of a large scale advanced turboprop rotor blade. This 8-blade rotor is designed to operate at Mach 0. 8 at an altitude of 35,000 ft. The blades are highly swept and twisted and of spar/shell constru ...
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Report
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August 1, 1984
The steady state displacements of a rotating advanced turboprop are computed using the geometrically nonlinear capabilities of COSMIC NASTRAN Rigid Format 4 and MSC NASTRAN Solution 64. A description of the modified Newton-Raphson algorithm used by Solutio ...
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