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Showing 1 - 6 of 6 results
Search Results
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 |
A wind tunnel investigation of three NACA 1-series inlets at Mach numbers up to 0.92
| Location | Call # | Status |
|---|---|---|
| Joyner - Microforms B300 | NAS 1.15:110300 | ✔ Available |
Wind tunnel investigation of three axisymmetric cowls of different lengths at Mach numbers from 0.60 to 0.92
| Location | Call # | Status |
|---|---|---|
| Joyner - Microforms B300 | NAS 1.15:4488 | ✔ Available |
An investigation of several NACA 1-series inlets at Mach numbers from 0.4 to 1.29 for mass-flow ratios near 1.0
| Location | Call # | Status |
|---|---|---|
| Joyner - Fed Docs Stacks | ASK AT REFERENCE DESK | ✔ Available |