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 / Julio Chu and Pierce L. Lawing.
| Author/creator | Chu, Julio |
| Other author | Lawing, Pierce L. |
| Other author | United States. National Aeronautics and Space Administration. Scientific and Technical Information Division. |
| Format | Book |
| Publication Info | [Washington, DC] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; [Springfield, Va.] : [For sale by the National Technical Information Service], 1990. |
| Description | 1 volume. |
| Subjects |
| Series | NASA technical memorandum ; 4189 NASA technical memorandum 4189. ^A467613 |
| General note | Distributed to depository libraries in microfiche. |
| General note | Shipping list no.: 93-1213-M. |
| Reproduction note | Joyner- Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1993] 3 microfiches. |
| Other title | 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. |
| Other title | High-Reynolds-number test of a five-percent-thick low-aspect-ratio semispan wing in the Langley 0.3-meter transonic cryogenic tunnel, wind tunnel distributions. |
| GPO item number | 0830-D (MF) |
| Govt. docs number | NAS 1.15:4227 |
Availability
| Library | Location | Call Number | Status | Item Actions |
|---|---|---|---|---|
| Joyner | Microforms B300 | NAS 1.15:4227 | ✔ Available |