Add to ORKGGasdynamic analysis for the turbine blades and nozzle vanes, HPFTP turbine analysis, and HPOTP turbine analysis are provided
Presentations were made concerning the development of design analysis tools for combustor liners, tu...
A description of the facility and turbine test rig is presented. Also discussed is the turbine cooli...
Finite-element, transient heat transfer analyses were performed for the first-stage blades of the sp...
Gasdynamic environments applied to the turbine blades and nozzles of the HPFTP and HPOTP were analyz...
Low pressure fuel turbopump turbine labyrinth send tip rubbing analysis, gas dynamic analysis, and H...
The model generation and structural analysis performed for the High Pressure Oxidizer Turbopump (HPO...
This volume summarizes the analysis used to assess the structural life of the Space Shuttle Main Eng...
The analysis performed on the High Pressure Oxidizer Turbopump (HPOTP) preburner pump bearing assemb...
Three dimensional nonlinear finite element heat transfer and structural analyses were performed for ...
The objective is to provide improved analysis capability for the Space Shuttle Main Engine (SSME) hi...
A simulation study was conducted to examine the transient rotordynamics of the space shuttle main en...
Space Shuttle Main Engine power spectra and dynamic pressure measurements from hot test firing are r...
Thermal and structural finite-element analyses were performed on the first high pressure fuel turbop...
To improve the Space Shuttle Main Engine (SSME) design and for future use in the development of gene...
This structural dynamic analysis supports development of the SSME by evaluating components subjected...
Presentations were made concerning the development of design analysis tools for combustor liners, tu...
A description of the facility and turbine test rig is presented. Also discussed is the turbine cooli...
Finite-element, transient heat transfer analyses were performed for the first-stage blades of the sp...
Gasdynamic environments applied to the turbine blades and nozzles of the HPFTP and HPOTP were analyz...
Low pressure fuel turbopump turbine labyrinth send tip rubbing analysis, gas dynamic analysis, and H...
The model generation and structural analysis performed for the High Pressure Oxidizer Turbopump (HPO...
This volume summarizes the analysis used to assess the structural life of the Space Shuttle Main Eng...
The analysis performed on the High Pressure Oxidizer Turbopump (HPOTP) preburner pump bearing assemb...
Three dimensional nonlinear finite element heat transfer and structural analyses were performed for ...
The objective is to provide improved analysis capability for the Space Shuttle Main Engine (SSME) hi...
A simulation study was conducted to examine the transient rotordynamics of the space shuttle main en...
Space Shuttle Main Engine power spectra and dynamic pressure measurements from hot test firing are r...
Thermal and structural finite-element analyses were performed on the first high pressure fuel turbop...
To improve the Space Shuttle Main Engine (SSME) design and for future use in the development of gene...
This structural dynamic analysis supports development of the SSME by evaluating components subjected...
Presentations were made concerning the development of design analysis tools for combustor liners, tu...
A description of the facility and turbine test rig is presented. Also discussed is the turbine cooli...
Finite-element, transient heat transfer analyses were performed for the first-stage blades of the sp...