Static performance of a fixed-geometry exhaust nozzle incorporating porous cavities for shock-boundary layer interaction control / Scott C. Asbury and Craig A. Hunter.
| Author/creator | Asbury, Scott C. author. |
| Other author | Hunter, Craig A. (Craig Allen), author. |
| Other author | Langley Research Center, issuing body. |
| Format | Electronic |
| Publication | Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, August 1999. |
| Description | 1 online resource (134 pages) : illustrations. |
| Supplemental Content | https://purl.fdlp.gov/GPO/gpo84477 |
| Series | NASA/TM ; 1999-209513 NASA technical memorandum 1999-209513. ^A467613 |
| General note | "August 1999." |
| General note | "Performing organization: NASA Langley Research Center"--Report documentation page. |
| General note | CRDP Program record. |
| Bibliography note | Includes bibliographical references (pages 19-20). |
| Report note | Technical memorandum. |
| Funding information | Sponsored by the National Aeronautics and Space Administration WU 538-14-12-01 L-17879 |
| Source of description | Description based on online resource; title from PDF title page (NASA, viewed Sep. 6, 2017). |
| Issued in other form | Print version: Asbury, Scott C. Static performance of a fixed-geometry exhaust nozzle incorporating porous cavities for shock-boundary layer interaction control |
| Issued in other form | Microfiche version: Asbury, Scott C. Static performance of a fixed-geometry exhaust nozzle incorporating porous cavities for shock-boundary layer interaction control |
| GPO item number | 0830-D (online) |
| Govt. docs number | NAS 1.15:209513 |
Availability
| Library | Location | Call Number | Status | Item Actions |
|---|---|---|---|---|
| Electronic Resources | Access Content Online | ✔ Available |