Add to ORKGDesign considerations, objectives, and approaches used in containing rotor burst debris are discussed. Methods are given for determining the fracture resistance of various materials used in providing lightweight shielding from fragment impact
The Federal Aviation Administration (FAA) is working with the European Aviation Safety Agency to det...
Rotor health monitoring and online damage detection are increasingly gaining the interest of the man...
Dimensional analysis techniques are described and applied to the containment/deflection problem of b...
Sections of the U.S. Airworthiness Standards which contribute to rotor integrity are explored. Repor...
A program to develop criteria for the design of devices that will be used on aircraft to protect pas...
Based on FAA data, results are presented that establish (1) the incidence of rotor failure, (2) the ...
A set of hypotheses is established as to what variables might control the design of a weight-efficie...
Statistical information relating to the number of gas turbine engine rotor failures which occurred d...
Statistics on gas turbine rotor failures that have occurred in U.S. commercial aviation during 1975 ...
This report presents statistical information relating to the number of gas turbine engine rotor fail...
Results of analytical studies to improve the low cycle fatigue lives and reliability of turbine disk...
The Federal Aviation Administration is working with the European Aviation Safety Agency to determine...
Recently, National Aeronautics and Space Administration (NASA) initiated a program to achieve the si...
AbstractThe potential hazard resulting from uncontained turbine engine rotor blade failure has alway...
https://doi.org/10.21949/14034641997PDFTech ReportDOT/FAA/AR-96/121RotorsTurbine enginesEnginesNacel...
The Federal Aviation Administration (FAA) is working with the European Aviation Safety Agency to det...
Rotor health monitoring and online damage detection are increasingly gaining the interest of the man...
Dimensional analysis techniques are described and applied to the containment/deflection problem of b...
Sections of the U.S. Airworthiness Standards which contribute to rotor integrity are explored. Repor...
A program to develop criteria for the design of devices that will be used on aircraft to protect pas...
Based on FAA data, results are presented that establish (1) the incidence of rotor failure, (2) the ...
A set of hypotheses is established as to what variables might control the design of a weight-efficie...
Statistical information relating to the number of gas turbine engine rotor failures which occurred d...
Statistics on gas turbine rotor failures that have occurred in U.S. commercial aviation during 1975 ...
This report presents statistical information relating to the number of gas turbine engine rotor fail...
Results of analytical studies to improve the low cycle fatigue lives and reliability of turbine disk...
The Federal Aviation Administration is working with the European Aviation Safety Agency to determine...
Recently, National Aeronautics and Space Administration (NASA) initiated a program to achieve the si...
AbstractThe potential hazard resulting from uncontained turbine engine rotor blade failure has alway...
https://doi.org/10.21949/14034641997PDFTech ReportDOT/FAA/AR-96/121RotorsTurbine enginesEnginesNacel...
The Federal Aviation Administration (FAA) is working with the European Aviation Safety Agency to det...
Rotor health monitoring and online damage detection are increasingly gaining the interest of the man...
Dimensional analysis techniques are described and applied to the containment/deflection problem of b...