Add to ORKGA set of hypotheses is established as to what variables might control the design of a weight-efficient protective device. A particular experiment for evaluating the hypotheses and materials was designed. The design and methods for the analysis of results are described
The development of theoretical rotor blade structural models for designs based upon composite constr...
An effective design methodology was established for composite jet engine containment structures. The...
Experimental and analytical investigations were conducted to evaluate a bearingless helicopter rotor...
Published results on rotor burst containment with single materials, and on body armor using composit...
Developed a lightweight containment system for high-speed composite rotors. The containment device, ...
Design considerations, objectives, and approaches used in containing rotor burst debris are discusse...
The Federal Aviation Administration is working with the European Aviation Safety Agency to determine...
Flywheel safety and containment design technology are discussed. The effects of axial loading result...
0088068837656374https://doi.org/10.21949/14037701997Final reportPDFTech ReportDOT/FAA/AR-96/110;AIR-...
The use of composites in fan blade containment systems is investigated and the associated structural...
Parametric type data were obtained on advanced lightweight containment systems. These data were used...
The development of containment concepts for use with large composite fan blades, taking into account...
Results are presented from the U.S. Army-Aerostructures Directorate/NASA-Langley Research Center joi...
A methodology is developed to perform minimum weight structural design for composite or metallic mai...
An integrated team of NASA personnel, Government contractors, industry partners, and university staf...
The development of theoretical rotor blade structural models for designs based upon composite constr...
An effective design methodology was established for composite jet engine containment structures. The...
Experimental and analytical investigations were conducted to evaluate a bearingless helicopter rotor...
Published results on rotor burst containment with single materials, and on body armor using composit...
Developed a lightweight containment system for high-speed composite rotors. The containment device, ...
Design considerations, objectives, and approaches used in containing rotor burst debris are discusse...
The Federal Aviation Administration is working with the European Aviation Safety Agency to determine...
Flywheel safety and containment design technology are discussed. The effects of axial loading result...
0088068837656374https://doi.org/10.21949/14037701997Final reportPDFTech ReportDOT/FAA/AR-96/110;AIR-...
The use of composites in fan blade containment systems is investigated and the associated structural...
Parametric type data were obtained on advanced lightweight containment systems. These data were used...
The development of containment concepts for use with large composite fan blades, taking into account...
Results are presented from the U.S. Army-Aerostructures Directorate/NASA-Langley Research Center joi...
A methodology is developed to perform minimum weight structural design for composite or metallic mai...
An integrated team of NASA personnel, Government contractors, industry partners, and university staf...
The development of theoretical rotor blade structural models for designs based upon composite constr...
An effective design methodology was established for composite jet engine containment structures. The...
Experimental and analytical investigations were conducted to evaluate a bearingless helicopter rotor...