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Applied Mechanics Commons™

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1999

Articles 1 - 6 of 6

Full-Text Articles in Applied Mechanics

Sept 1999, Tractor Museum Sep 1999

Sept 1999, Tractor Museum

Lester F. Larsen Tractor Museum: Planning and Development Documents

Director's Report Curator's Report Friend's Letterhead and Logo

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Triangulation Rangefinder And Sight Positioning System, Jeffrey Hargrove, William G. Wickham, John E. Briggs Jun 1999

Triangulation Rangefinder And Sight Positioning System, Jeffrey Hargrove, William G. Wickham, John E. Briggs

Mechanical Engineering Patents

A rangefinder includes an angle sensitive transducer and a programmed data processor to calculate the distance to a target. In one embodiment, the rangefinder also includes a point-to-point measuring device. Another embodiment provides a linear actuator to selectively move a sight indicator vertically. A yet additional embodiment includes a liquid crystal display which displays information to the user.

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Jun 1999, Tractor Museum Jun 1999

Jun 1999, Tractor Museum

Lester F. Larsen Tractor Museum: Planning and Development Documents

Foundation Account Friends of NE State Museum Newsletter

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Mar 1999, Tractor Museum Mar 1999

Mar 1999, Tractor Museum

Lester F. Larsen Tractor Museum: Planning and Development Documents

Additional Funds Donation to Camp Creek Threshers Renovation Status

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Jan 1999, Tractor Museum Jan 1999

Jan 1999, Tractor Museum

Lester F. Larsen Tractor Museum: Planning and Development Documents

Museum Open House Officer Elections UN Museum

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Multidisciplinary Sensitivity Analysis And Design Optimization Of Flexible Wings Using The Euler Equations On Unstructured Grids, Arunkumar Satyanarayana Jan 1999

Multidisciplinary Sensitivity Analysis And Design Optimization Of Flexible Wings Using The Euler Equations On Unstructured Grids, Arunkumar Satyanarayana

Mechanical & Aerospace Engineering Theses & Dissertations

Aeroelasticity is a classical discipline. However, even with recent advancement in computational technology, it still remains a challenging discipline. This is particularly true when aeroelasticity problems are solved in a loosely coupled manner. The advantage of a loosely coupled scheme is that the legacy codes of computational fluid dynamics (CFD) and computational structural mechanics (CSM) can be preserved and used as independent modules in solving the desired aeroelasticity problems. In such a scheme, maintaining proper data transfer (load transfer and deformation tracking between CFD and CSM codes) is crucial in ensuring successful coupled solutions. This can be a challenging task …

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