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Experimental investigation of wing installation effects on a two-dimensional mixer/ejector nozzle for supersonic transport aircraft
| Location | Call # | Status |
|---|---|---|
| Joyner - Microforms B300 | NAS 1.15:105713 | ✔ Available |
Highly integrated digital engine control system on an NASA F-15 airplane
| Location | Call # | Status |
|---|---|---|
| Joyner - Microforms B300 | NAS 1.15:86040 | ✔ Available |
Static internal performance of a two-dimensional convergent-divergent nozzle with external shelf
| Location | Call # | Status |
|---|---|---|
| Joyner - Microforms B300 | NAS 1.15:4719 | ✔ Available |
1999 NASA High-Speed Research Program Aerodynamic Performance Workshop
| Location | Call # | Status |
|---|---|---|
| Joyner - Microforms B300 | NAS 1.55:209704/V.1/PT.1- | ✔ Available |