The results of a 20-month program, designed to investigate parameters which effect the foreign object damage resulting from ingestion of birds into fan blades are described. Work performed on this program included the design, fabrication, and impact testing of QCSEE fan blades to demonstrate improvement in resistance relative to existing blades and also the design and demonstration of a pin root attachment concept
Structural and dynamic analyses are presented for a shroudless, hollow titanium fan blade proposed f...
Results of tests conducted on preliminary design polymeric-composite fan blade for the under the win...
Efforts to improve the impact resistance of B/Al are reviewed and analyzed. Thin sheet Charpy and Iz...
Results are presented of a program to determine the impact resistance of composite fan blades subjec...
Boron/epoxy and graphite/epoxy composite blades were impacted in a rotating whirligig facility with ...
The results of impact tests on large, fiber composite fan blades for aircraft turbofan engine applic...
Six filament-wound, composite spar-shell fan blades were impact tested in a whirligig relative to fo...
Composite spar-shell fan blades for a 1.83 meter (6 feet) diameter fan stage were fabricated and tes...
The development of containment concepts for use with large composite fan blades, taking into account...
Processing procedures were developed to enhance boron/aluminum bond behavior and foreign object dama...
The technical program was comprised of two technical tasks. Task 1 encompassed the preliminary boron...
Application of polymer matrix composite materials for jet engine fan blades is becoming attractive a...
Improved resistance to foreign object damage was demonstrated for hybrid composite simulated blade s...
The theoretical methodology used in developing an analysis for the response of turbine engine fan bl...
Recent developments in the analysis of high velocity impact of composite blades are described, using...
Structural and dynamic analyses are presented for a shroudless, hollow titanium fan blade proposed f...
Results of tests conducted on preliminary design polymeric-composite fan blade for the under the win...
Efforts to improve the impact resistance of B/Al are reviewed and analyzed. Thin sheet Charpy and Iz...
Results are presented of a program to determine the impact resistance of composite fan blades subjec...
Boron/epoxy and graphite/epoxy composite blades were impacted in a rotating whirligig facility with ...
The results of impact tests on large, fiber composite fan blades for aircraft turbofan engine applic...
Six filament-wound, composite spar-shell fan blades were impact tested in a whirligig relative to fo...
Composite spar-shell fan blades for a 1.83 meter (6 feet) diameter fan stage were fabricated and tes...
The development of containment concepts for use with large composite fan blades, taking into account...
Processing procedures were developed to enhance boron/aluminum bond behavior and foreign object dama...
The technical program was comprised of two technical tasks. Task 1 encompassed the preliminary boron...
Application of polymer matrix composite materials for jet engine fan blades is becoming attractive a...
Improved resistance to foreign object damage was demonstrated for hybrid composite simulated blade s...
The theoretical methodology used in developing an analysis for the response of turbine engine fan bl...
Recent developments in the analysis of high velocity impact of composite blades are described, using...
Structural and dynamic analyses are presented for a shroudless, hollow titanium fan blade proposed f...
Results of tests conducted on preliminary design polymeric-composite fan blade for the under the win...
Efforts to improve the impact resistance of B/Al are reviewed and analyzed. Thin sheet Charpy and Iz...