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Search Results
Results of S5 CH tests with an ARL (Aerospace Research Laboratory) cascade
| Location | Call # | Status |
|---|---|---|
| Joyner - Microforms B300 | NAS 1.15:77510 | ✔ Available |
Subsonic and transonic pressure measurements on a high-aspect-ratio supercritical-wing model with oscillating control surfaces
| Location | Call # | Status |
|---|---|---|
| Joyner - Microforms B300 | NAS 1.15:83201 | ✔ Available |
Computer model to simulate testing at the National Transonic Facility
| Location | Call # | Status |
|---|---|---|
| Joyner - Microforms B300 | NAS 1.15:4664 | ✔ Available |
Sea level static calibration of a compact multimission aircraft propulsion simulator with inlet flow distortion
| Location | Call # | Status |
|---|---|---|
| Joyner - Microforms B300 | NAS 1.15:102838 | ✔ Available |
A two-dimensional adaptive-wall test section with ventilated walls in the Ames 2- by 2-foot transonic wind tunnel
| Location | Call # | Status |
|---|---|---|
| Joyner - Microforms B300 | NAS 1.15:102207 | ✔ Available |
Operating capability and current status of the reactivated NASA Lewis Research Center hypersonic tunnel facility
| Location | Call # | Status |
|---|---|---|
| Joyner - Microforms B300 | NAS 1.15:106808 | ✔ Available |
Unsteady velocity measurements taken behind a model helicopter rotor hub in forward flight
| Location | Call # | Status |
|---|---|---|
| Joyner - Microforms B300 | NAS 1.15:4738 | ✔ Available |
Static wind-tunnel and radio-controlled flight test investigation of a remotely piloted vehicle having a delta wing planform
| Location | Call # | Status |
|---|---|---|
| Joyner - Microforms B300 | NAS 1.15:4200 | ✔ Available |