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Full-Text Articles in Engineering
The Application Of Limit Analysis To Shell Structures Using Existing Finite Element Analysis Codes, George G. Myers
The Application Of Limit Analysis To Shell Structures Using Existing Finite Element Analysis Codes, George G. Myers
Retrospective Theses and Dissertations
A ramjet inlet duct structure has been designed using nonlinear structural analysis to allow local plastic deformations which result in structural weight reduction. To establish the feasibility of reduced shell thickness, the Lower-Bound Theorem of limit analysis has been applied using an existing finite element analysis computer code intended for elastic analysis. The results of the analysis were verified by structural testing. Predicted stresses and deflections showed good correlation with measured values up to the point of failure. This work was supported by the U.S. Air Force Aero Propulsion Laboratory, Wright-Patterson Air Force Base, Ohio, under Contract No. F33615-72-C-1366.
Nose Tip Recession Measuring System For Hypersonic Test Vehicles, James Anthony Brown
Nose Tip Recession Measuring System For Hypersonic Test Vehicles, James Anthony Brown
Retrospective Theses and Dissertations
A method is presented which permits the measure of nose tip recession of re-entry vehicles and advanced terminal interceptors by employing a double choked flow coolant gas system. Recession of the tip results in an increased exit flow area which reduces the total pressure of the gas in the blast tube. Measurement of the blast tube pressure and gas generator (chamber) pressure will produce an effective measurement of the nose tip recession as long as choked flow (i.e., sonic velocity) is maintained in both the tip exit area and the gas generator throat area. Governing flow equations documented in the …