Add to ORKGA detailed stress analysis was performed using NASTRAN to demonstrate theoretically the adequacy of composite hubs for low cost turbine engine applications. Composite hubs are adequate for this application from the steady state stress view point
Seven composite engines were designed for application to a reusable single-stage-to-orbit vehicle. T...
A theoretical investigation was performed to determine the structural response of a fiber composite ...
This paper deals with the design of the carbon fibre composite driveshaft. This driveshaft will be u...
Elementary relations are described to determine the material utilization efficiency of a thin wall r...
Design concepts for low-cost, lightweight composite engine frames were applied to the design require...
Composite component designs were developed for a number of applicable engine parts and functions. Th...
Results from a number of studies concerned with the cost and benefits of applying advanced composite...
A program was conducted by NASA with the JT9D engine manufacturer to develop a lightweight, cost eff...
The paper addresses some of the issues involved in the development of an all-composite aero gasturbi...
The Low Cost Booster Technology Program is an initiative to minimize the cost of future liquid engin...
A composite hub was successfully designed and fabricated for a flywheel rotor of 51 kWh energy stora...
Design concepts for low cost, lightweight composite engine frames were applied to the design require...
An integrated team of NASA personnel, Government contractors, industry partners, and university staf...
The Lewis Research Center is conducting a series of programs intended to investigate and develop the...
A series of programs were conducted to investigate and develop the application of composite material...
Seven composite engines were designed for application to a reusable single-stage-to-orbit vehicle. T...
A theoretical investigation was performed to determine the structural response of a fiber composite ...
This paper deals with the design of the carbon fibre composite driveshaft. This driveshaft will be u...
Elementary relations are described to determine the material utilization efficiency of a thin wall r...
Design concepts for low-cost, lightweight composite engine frames were applied to the design require...
Composite component designs were developed for a number of applicable engine parts and functions. Th...
Results from a number of studies concerned with the cost and benefits of applying advanced composite...
A program was conducted by NASA with the JT9D engine manufacturer to develop a lightweight, cost eff...
The paper addresses some of the issues involved in the development of an all-composite aero gasturbi...
The Low Cost Booster Technology Program is an initiative to minimize the cost of future liquid engin...
A composite hub was successfully designed and fabricated for a flywheel rotor of 51 kWh energy stora...
Design concepts for low cost, lightweight composite engine frames were applied to the design require...
An integrated team of NASA personnel, Government contractors, industry partners, and university staf...
The Lewis Research Center is conducting a series of programs intended to investigate and develop the...
A series of programs were conducted to investigate and develop the application of composite material...
Seven composite engines were designed for application to a reusable single-stage-to-orbit vehicle. T...
A theoretical investigation was performed to determine the structural response of a fiber composite ...
This paper deals with the design of the carbon fibre composite driveshaft. This driveshaft will be u...