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Flight test results of riblets at supersonic speeds
| Location | Call # | Status |
|---|---|---|
| Joyner - Microforms B300 | NAS 1.15:4387 | ✔ Available |
Effects of wing sweep on in-flight boundary-layer transition for a laminar flow wing at Mach numbers from 0.60 to 0.79
| Location | Call # | Status |
|---|---|---|
| Joyner - Microforms B300 | NAS 1.15:101701 | ✔ Available |
Effects of wing sweep on boundary-layer transition for a smooth F-14A wing at Mach numbers from 0.700 to 0.825
| Location | Call # | Status |
|---|---|---|
| Joyner - Microforms B300 | NAS 1.15:101712 | ✔ Available |