Parametric type data were obtained on advanced lightweight containment systems. These data were used to generate design methods and procedures necessary for the successful development of such systems. The methods were then demonstrated through the design of a lightweight containment system for a CF6 size engine. The containment concept evaluated consisted basically of a lightweight structural sandwich shell wrapped with dry Kevlar cloth. The initial testing was directed towards the determination of the amount of Kevlar required to result in threshold containment for a specific set of test conditions. A relationship was then developed between the thickness required and the energy of the released blade so that the data could be used to design...
Design, manufacture and testing of laminated and coated composite materials incorporating a structur...
The detail design of the under the wing experimental composite nacelle components is summarized. Ana...
Current activities in seals for space propulsion turbomachinery that the NASA Lewis Research Center ...
A set of hypotheses is established as to what variables might control the design of a weight-efficie...
A lightweight containment was developed for turbofan engine fan blades. Subscale ballistic-type test...
A cylindrical shell structure 3.66 m (144 in.) high by 4.57 m (180 in.) diameter was designed using ...
Developed a lightweight containment system for high-speed composite rotors. The containment device, ...
The use of composites in fan blade containment systems is investigated and the associated structural...
0088068837656374https://doi.org/10.21949/14037701997Final reportPDFTech ReportDOT/FAA/AR-96/110;AIR-...
An integrated team of NASA personnel, Government contractors, industry partners, and university staf...
The Federal Aviation Administration is working with the European Aviation Safety Agency to determine...
Lightweight external panel insulation systems for thermal protection of cryogenic launch vehicle pro...
Structural sealing problems and leakage rates of lightweight simulated spacecraft air lock under hig...
This is an overview presentation of research being performed in the Advanced Materials Task within t...
An advanced lightweight insulation system suitable for use in long duration, low pressure planetary ...
Design, manufacture and testing of laminated and coated composite materials incorporating a structur...
The detail design of the under the wing experimental composite nacelle components is summarized. Ana...
Current activities in seals for space propulsion turbomachinery that the NASA Lewis Research Center ...
A set of hypotheses is established as to what variables might control the design of a weight-efficie...
A lightweight containment was developed for turbofan engine fan blades. Subscale ballistic-type test...
A cylindrical shell structure 3.66 m (144 in.) high by 4.57 m (180 in.) diameter was designed using ...
Developed a lightweight containment system for high-speed composite rotors. The containment device, ...
The use of composites in fan blade containment systems is investigated and the associated structural...
0088068837656374https://doi.org/10.21949/14037701997Final reportPDFTech ReportDOT/FAA/AR-96/110;AIR-...
An integrated team of NASA personnel, Government contractors, industry partners, and university staf...
The Federal Aviation Administration is working with the European Aviation Safety Agency to determine...
Lightweight external panel insulation systems for thermal protection of cryogenic launch vehicle pro...
Structural sealing problems and leakage rates of lightweight simulated spacecraft air lock under hig...
This is an overview presentation of research being performed in the Advanced Materials Task within t...
An advanced lightweight insulation system suitable for use in long duration, low pressure planetary ...
Design, manufacture and testing of laminated and coated composite materials incorporating a structur...
The detail design of the under the wing experimental composite nacelle components is summarized. Ana...
Current activities in seals for space propulsion turbomachinery that the NASA Lewis Research Center ...