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Impingement of boundary-reflected disturbances originating at the nose of a body of revolution in the Langley Research Center 16-foot transonic tunnel
| Location | Call # | Status |
|---|---|---|
| Joyner - Microforms B300 | NAS 1.15:208723 | ✔ Available |
Static internal performance of an axisymmetric nozzle with multiaxis thrust-vectoring capability
| Location | Call # | Status |
|---|---|---|
| Joyner - Microforms B300 | NAS 1.15:4237 | ✔ Available |
Effects of nozzle exit location and shape on propulsion-induced aerodynamic characteristics due to vectoring twin nozzles at Mach numbers from 0.4 ̥to 1.2
| Location | Call # | Status |
|---|---|---|
| Joyner - Fed Docs Stacks | ASK AT REFERENCE DESK | ✔ Available |