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The construction of airfoil pressure models by the bonded plate method
| Location | Call # | Status |
|---|---|---|
| Joyner - Microforms B300 | NAS 1.15:87613 | ✔ Available |
High-Reynolds-number test of a 5-percent-thick low-aspect-ratio semispan wing in the Langley 0.3-meter transonic cryogenic tunnel, wing tunnel distributions
| Location | Call # | Status |
|---|---|---|
| Joyner - Microforms B300 | NAS 1.15:4227 | ✔ Available |