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. |
| Other author | Hunter, Craig A. (Craig Allen) |
| Other author | Langley Research Center. |
| Format | Microform |
| Publication Info | Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va.] : [National Technical Information Service, distributor], [1999] |
| Description | 1 volume. |
| Series | NASA/TM ; 1999-209513 NASA technical memorandum 209513. ^A467613 |
| General note | Shipping list no.: 2000-0197-M. |
| General note | CRDP Program record. |
| Reproduction note | Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1999]. 2 microfiches. |
| 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 | Online 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 (MF) |
| Govt. docs number | NAS 1.15:209513 |
| Stock number | 19990100650 NASA |
Availability
| Library | Location | Call Number | Status | Item Actions |
|---|---|---|---|---|
| Joyner | Microforms B300 | NAS 1.15:209513 | ✔ Available |