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Overall and blade element performance of a 1.20-pressure-ratio fan stage with rotor blades reset -5 ̊
| Location | Call # | Status |
|---|---|---|
| Joyner - Fed Docs Stacks | ASK AT REFERENCE DESK | ✔ Available |
Overall and blade element performance of a 1.20 pressure ratio fan stage with rotor blades reset -7 ̊
| Location | Call # | Status |
|---|---|---|
| Joyner - Fed Docs Stacks | ASK AT REFERENCE DESK | ✔ Available |
A comparison of sound power levels from portable air compressors based upon test methodologies adopted by U.S. EPA and the CEC
| Location | Call # | Status |
|---|---|---|
| Joyner - Fed Docs Stacks | EP 1.2:SO 8/14 | ✔ Available |
JTAGG II brush seal test results
| Location | Call # | Status |
|---|---|---|
| Joyner - Microforms B300 | NAS 1.15:107448 | ✔ Available |
Forced response testing of an axi-centrifugal turboshaft engine
| Location | Call # | Status |
|---|---|---|
| Joyner - Microforms B300 | NAS 1.15:107282 | ✔ Available |
Relative performance comparison between baseline labyrinth and dual-brush compressor discharge seals in a T-700 engine test
| Location | Call # | Status |
|---|---|---|
| Joyner - Microforms B300 | NAS 1.15:106360 | ✔ Available |
Brush seal performance and durability issues based on T-700 engine test results
| Location | Call # | Status |
|---|---|---|
| Joyner - Microforms B300 | NAS 1.15:106502 | ✔ Available |