Surface-pressure and flow-visualization data at Mach number of 1.60 for three 65° delta wings varying in leading-edge radius and camber / S. Naomi McMillin [and five others].
| Author/creator | McMillin, S. Naomi author. |
| Other author | Langley Research Center, issuing body. |
| Other author | United States. National Aeronautics and Space Administration sponsoring body. |
| Format | Electronic |
| Publication | Hampton, VA : National Aeronautics and Space Administration, Langley Research Center, December 1996. |
| Description | 1 online resource (iii, 262 pages) : illustrations. |
| Supplemental Content | https://purl.fdlp.gov/GPO/gpo65356 |
| Series | NASA technical memorandum ; 4673 NASA technical memorandum 4673. ^A467613 |
| General note | Title from title screen (viewed March 2, 2016). |
| General note | "December 1996." |
| General note | "Performing organization: NASA Langley Research Center, Hampton, VA"--Report documentation page. |
| General note | GPO Cataloging Record Distribution Program (CRDP). |
| Bibliography note | Includes bibliographical references (page 262). |
| Funding information | Sponsored by the National Aeronautics and Space Administration WU 505-59-53-05 L-17443 |
| Issued in other form | Print version: Surface-pressure and flow-visualization data at Mach number of 1.60 for three 65° delta wings varying in leading-edge radius and camber |
| Issued in other form | Microfiche version: Surface-pressure and flow-visualization data at Mach number of 1.60 for three 65 ̊delta wings varying in leading-edge radius and camber |
| GPO item number | 0830-D (online) |
| Govt. docs number | NAS 1.15:4673 |
Availability
| Library | Location | Call Number | Status | Item Actions |
|---|---|---|---|---|
| Electronic Resources | Access Content Online | ✔ Available |